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Langley Research Center
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The organization ** Langley Research Center** represents an institution, an association, or corporate body that is associated with resources found in **San Francisco Public Library**.

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Langley Research Center
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**Langley Research Center**represents an institution, an association, or corporate body that is associated with resources found in**San Francisco Public Library**.- Label
- Langley Research Center

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- 14- by 22-foot subsonic tunnel laser velocimeter upgrade
- 1984 direct strike lightning data
- 3D space radiation transport in a shielded ICRU tissue sphere
- 3DHZETRN : inhomogeneous geometry issues
- 4D dynamic required navigation performance final report
- A 3DHZETRN code in a spherical uniform sphere with Monte Carlo verification
- A Riemann solver based on a global existence proof for the Riemann problem
- A System for aerodynamic design and analysis of supersonic aircraft
- A Web-based system for monitoring and controlling multidisciplinary design projects
- A back face strain compliance expression for the compact tension specimen
- A benchmark problem for development of autonomous structural modal identification
- A benefit analysis of infusing wireless into aircraft and fleet operations : report to seedling project efficient reconfigurable cockpit design and fleet operations using software intensive, network enabled, wireless architecture (ECON)
- A candidate wake vortex strength definition for application to the NASA Aircraft Vortex Spacing System (AVOSS)
- A case study on the application of a structured experimental method for optimal parameter design of a complex control system
- A clamped rectangular plate containing a crack
- A cockpit-display concept for executing a multiple glide-slope approach for wake-vortex avoidance
- A combined integrating and differentiating matrix formulation for boundary value problems on rectangular domains
- A compact efficient lidar receiver for measuring atmospheric aerosols
- A comparison of analytical and experimental data for a magnetic actuator
- A comparison of pressure measurements between a full-scale and a 1/6-scale F/A-18 twin tail during buffet
- A comparison of signal enhancement methods for extracting tonal acoustic signals
- A comparison of three random number generators for aircraft dynamic modeling applications
- A comparison of two control display unit concepts on flight management system training
- A compilation of Space Shuttle sonic boom measurements
- A comprehensive analysis of the X-15 flight 3-65 accident
- A computational approach for probabilistic analysis of water impact simulations
- A computer program for the generation of logic networks from task chart data
- A concept for airborne precision spacing for dependent parallel approaches
- A concept for flexible operations and optimized traffic into metroplex regions
- A coupled probabilistic wake vortex and aircraft response prediction model
- A criteria standard for conflict resolution : a vision for guaranteeing the safety of self-separation in NextGen
- A critical comparison of turbulence models for homogeneous shear flows in a rotating frame
- A critique of a phenomenological fiber breakage model for stress rupture of composite materials
- A data system for a rapid evaluation class of subscale aerial vehicle
- A deployable primary mirror for space telescopes
- A discussion of zero spring rate mechanisms used for the active isolation mount experiment
- A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-Meter Transonic Cryogenic Tunnel
- A fault injection experiment using the airlab diagnostic emulation facility
- A feasibility study to control airfoil shape using THUNDER
- A formally-verified decision procedure for univariate polynomial computation based on Sturm's Theorem
- A fourth-order scheme for the unsteady compressibile Navier-Stokes equations
- A general formalism for phase space calculations
- A high-level formalization of floating-point numbers in PVS
- A high-order Lagrangian-decoupling method for the incompressible Navier-Stokes equations
- A launch requirements trade study for active space radiation shielding for long duration human missions
- A method for the reduction of aerodynamic drag of road vehicles
- A method of boundary parameter estimation for a two-dimensional diffusion system under noisy observations
- A method to stabilize linear systems using eigenvalue gradient information
- A methodology for the design and verification of globally asynchronous/locally synchronous architectures
- A multidisciplinary tool for systems analysis of planetary entry, descent, and landing (SAPE)
- A new look at numerical analyses of free-edge stresses in composite laminates
- A new method for reduction of photomultiplier signal-induced noise
- A new theory for rapid calculation of the ground pattern of the incident sound intensity produced by a maneuvering jet airplane
- A note about HARP's state trimming method
- A numerical simulation of the dispersal of aerial sprays
- A parametric study of accelerations of an airplane due to a wake vortex system
- A partitioning strategy for non-uniform problems on multiprocessors
- A piloted simulator evaluation of transport aircraft rudder pedal force/feel characteristics
- A practical engineering approach to predicting fatigue crack growth in riveted lap joints
- A practical tutorial on modified condition/decision coverage
- A preliminary design for flight testing the FINDS algorithm
- A progressive damage methodology for residual strength predictions of notched composite panels
- A qualitative piloted evaluation of the Tupolev Tu-144 supersonic transport
- A rapid empirical method for estimating the gross takeoff weight of a high speed civil transport
- A review of current and prospective factors for classification of civil unmanned aircraft systems
- A review of function allocation and en route separation assurance
- A self-stabilizing distributed clock synchronization protocol for arbitrary digraphs
- A short tutorial on inertial navigation system and global positioning system integration
- A simple engineering analysis of solar particle event high energy tails and their impact on vehicle design
- A simple transient thermal test assembly for insulation materials
- A simulator study for the development and evaluation of operating procedures on a supersonic cruise research transport to minimize airport-community noise
- A state of-the-art experimental laboratory for cloud and cloud-aerosol interaction research : need for a national facility to complement in situ and remote field measurements for improved atmospheric modeling and simulation : background and discussion
- A storm surge and inundation model of the Back River watershed at NASA Langley Research Center
- A study in a new test facility on indoor annoyance caused by sonic booms
- A study of flexible composites for expandable space structures
- A study of neutron leakage in finite objects
- A study of shape memory polymer based slat-cove filler
- A study of the sonic-boom characteristics of a blunt body at a Mach number of 6
- A summary of results from two full-scale Fokker F28 fuselage section drop tests
- A summary of the Rendezvous, Proximity Operations, Docking, and Undocking (RPODU) lessons learned from the Defense Advanced Research Project Agency (DARPA) Orbital Express (OE) demonstration system mission
- A test for characterizing delamination migration in carbon/epoxy tape laminates
- A thermodynamically consistent damage model for advanced composites
- A tool for measuring NASA's aeronautics research progress toward planned strategic community outcomes
- A treatise on equivalent-plate stiffnesses for stiffened laminated-composite plates and plate-like lattices
- A turn-projected state-based conflict resolution algorithm
- A well-clear volume based on time to entry point
- A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92
- AF-Shell 1.0 user guide
- AFC-enabled simplified high-lift system integration study
- AFC-enabled vertical tail system integration study
- ATD occupant responses from three full-scale general aviation crash tests
- Accuracy of schemes for the Euler equations with nonuniform meshes
- Accuracy of schemes with nonuniform meshes for compressible fluid flows
- Achieving agreement in three rounds with bounded-Byzantine faults
- Acoustic performance of a real-time three-dimensional sound-reproduction system
- Acoustic radiation pressure
- Acoustically tailored composite rotorcraft fuselage panels
- Active control of compressible flow on a curved surface
- Active control of flow separation over an airfoil
- Adapting a Navier-Stokes code to the ICL-DAP
- Adaptive back sheet material for acoustics liner applications--ARMD Seedling Fund phase I final report
- Adaptive control in the presence of simultaneous sensor bias and actuator failures
- Adaptive control of large space structures using recursive lattice filters
- Adaptive identification and control of structural dynamics systems using recursive lattice filters
- Additive manufacturing modeling and simulation : a literature review for electron beam free form fabrication
- Advanced composite stabilizer for Boeing 737 aircraft
- Advanced information processing system : Input/output system services
- Advanced interval management (IM) concepts of operations
- Advanced small perturbation potential flow theory for unsteady aerodynamic and aeroelastic analyses
- Advanced-to-revolutionary space technology options : the responsibly imaginable
- Advances in fatigue and fracture mechanics analyses for metallic aircraft structures
- Aero-heating of shallow cavities in hypersonic freestream flow
- Aero-structural assessment of an inflatable aerodynamic decelerator
- Aeroacoustic codes for rotor harmonic and BVI noise - CAMRAD.Modl/HIRES : methodology and users' manual
- Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet
- Aerocapture systems analysis for a Titan mission
- Aerodynamic analysis for aircraft with nacelles, pylons, and winglets at transonic speeds
- Aerodynamic characteristics and control effectiveness of the HL-20 lifting body configuration at Mach 10 in air
- Aerodynamic characteristics of a hypersonic research airplane concept having a 70̊ swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0
- Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47
- Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90
- Aerodynamic characteristics of two NASA supercritical airfoils with different maximum thicknesses
- Aerodynamic design via control theory
- Aerodynamic measurements on a large splitter plate for the NASA Langley Transonic Dynamics Tunnel
- Aerodynamic parameters of an advanced fighter aircraft estimated from flight data : preliminary results
- Aeroelastic analyses of the SemiSpan Supersonic Transport (S4T) wind tunnel model at Mach 0.95
- Aeroelastic deformation : adaptation of wind tunnel measurement concepts to full-scale vehicle flight testing
- Aeroelastic sizing for high-speed research (HSR) longitudinal control alternatives project (LCAP)
- Aeroelastic tailoring of transport aircraft wings : state-of-the-art and potential enabling technologies
- Aeroelastic tailoring via tow steered composites
- Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20
- Aeroservoelastic testing of free flying wind tunnel models
- Aerothermal analysis and design of the Gravity Recovery and Climate Experiment (GRACE) spacecraft
- Aerothermal analysis of a wing-elevon cove with variable leakage
- Aerothermal environment in chordwise gaps between split elevons at Mach 6.8
- Air traffic management technology demonstration-1 concept of operations (ATD-1 ConOps)
- Air traffic management technology demonstration-1 concept of operations (ATD-1 ConOps), version 2.0
- Air traffic management technology demonstration-1 research and procedural testing of routes
- Air traffic management technology demostration phase 1 (ATD) interval management for near-term operations validation of acceptability (IM-NOVA) experiment
- Airborne forward-looking interferometer for the detection of terminal-area hazards
- Airborne precision spacing (APS) dependent parallel arrivals (DPA)
- Airborne precision spacing for dependent parallel operations interface study
- Airport traffic conflict detection and resolution algorithm evaluation
- Aladyn -- adaptive neural network molecular dynamics simulation code : computational materials mini-application
- Algorithm for simulating atmospheric turbulence and aeroelastic effects on simulator motion systems
- Alternate space station Freedom configuration considerations to accommodate solar dynamic power
- Alternative aviation fuel experiment (AAFEX)
- Amplitude noise reduction of ion lasers with optical feedback
- An Approximate solution and master curves for buckling of symmetrically laminated composite cylinders
- An advanced technology space station for the year 2025, study and concepts
- An aeroelastic analysis of helicopter rotor blades incorporating piezoelectric fiber composite twist actuation
- An airfoil flutter model suspension system to accomdate large static transonic airloads
- An amplitude-based estimation method for International Space Station (ISS) leak detection and localization using acoustic sensor networks
- An analysis of the speed commands from an interval management algorithm during the ATD-1 flight test
- An analytical method to calculate effective elastic properties of general multifunctional honeycomb cores in sandwich composites
- An analytical technique for approximating unsteady aerodynamics in the time domain
- An application of UAV attitude estimation using a low-cost inertial navigation system
- An application of the difference potentials method to solving external problems in CFD
- An approach for the assessment of system upset resilience
- An assessment of self-healing fiber reinforced composites
- An assessment of the state-of-the-art in the design and manufacturing of large composite structures for aerospace vehicles
- An asymptotic analysis of supersonic reacting mixing layers
- An automated DAKOTA and VULCAN-CFD framework with application to supersonic facility nozzle flowpath optimization
- An efficient sparse matrix multiplication scheme for the CYBER 205 computer
- An empirical study of flight control software reliability
- An enriched shell finite element for progressive damage simulation in composite laminates
- An evaluation of measured pressure signatures from wind-tunnel models of three low-boom concepts
- An evaluation of study designs for estimating a time-of-day noise weighting
- An evaluation of three experimental processes for two-dimensional transonic tests
- An examination of aviation accidents associated with turbulence, wind shear and thunderstorm
- An examination of launch vehicle loads reanalysis techniques
- An experimental investigation of a wing-fuselage junction model in the NASA Langley 14- by 22-foot subsonic tunnel
- An experimental investigation of damaged arresting gear tapes for the Langley Aircraft Landing Dynamics Facility
- An experimental investigation of the ground vortex created by a moving jet
- An experimental study of a stitched composite with a notch subjected to combined bending and tension loading
- An experimental study of fatigue crack growth in aluminum sheet subjected to combined bending and membrane stresses
- An exploratory investigation of a slotted, natural-laminar-flow airfoil
- An in-depth tutorial on constitutive equations for elastic anisotropic materials
- An initial study of the sensitivity of Aircraft Vortex Spacing System (AVOSS) spacing sensitivity to weather and configuration input parameters
- An integrating matrix formulation for buckling of rotating beams including the effects of concentrated masses
- An introduction to orbit dynamics and its application to satellite-based earth monitoring missions
- An introduction to requirements capture using PVS : specification of a simple autopilot
- An investigation at static conditions of nonaxisymmetric nozzle thrust reverser port geometry including effects of rounding and rotating the port corner
- An investigation of proposed techniques for quantifying confidence in assurance arguments
- An optimal repartitioning decision policy
- An overview of a trajectory-based solution for en route and terminal area self-spacing : fifth revision
- An overview of a trajectory-based solution for en route and terminal area self-spacing : fourth revision
- An overview of a trajectory-based solution for en route and terminal area self-spacing : seventh revision
- An overview of a trajectory-based solution for en route and terminal area self-spacing : sixth revision
- An overview of a trajectory-based solution for en route and terminal area self-spacing : third revision
- An overview of a trajectory-based solution for en route and terminal area self-spacing to include parallel runway operations
- An ozone differential absorption lidar (DIAL) receiver system for use on unpiloted atmospheric vehicles
- Analysis and simulation of the simplified aircraft-based paired approach concept with the ALAS alerting algorithm in conjunction with echelon and offset strategies
- Analysis and sizing for transient thermal heating of insulated aerospace vehicle structures
- Analysis and test of superplastically formed titanium hat-stiffened panels under compression
- Analysis methods for progressive damage of composite structures
- Analysis of a split-plot experimental design applied to a low-speed wind tunnel investigation
- Analysis of airborne antenna systems using geometrical theory of diffraction and moment method computer codes
- Analysis of dependencies and impacts of Metroplex Operations
- Analysis of flow dynamics through small diameter gas sampling systems
- Analysis of operational hazards and safety requirements for Traffic Aware Strategic Aircrew Requests (TASAR)
- Analysis of some acoustics-jet flow interaction problems
- Analysis of the radiated field in an electromagnetic reverberation chamber as an upset-inducing stimulus for digital systems
- Analysis of well-clear boundary models for the integration of UAS in the NAS
- Analysis of wind tunnel longitudinal static and oscillatory data of the F-16XL aircraft
- Analytic and computational perspectives of multi-scale theory for homogeneous, laminated composite, and sandwich beams and plates
- Analytic theory for the determination of velocity and stability of bubbles in a Hele-Shaw cell, Part II, Stability
- Analytical investigation of synchrophasing as a means of reducing aircraft interior noise
- Analytical methodology for predicting the onset of widespread fatigue damage in fuselage structure
- Analytical study of acoustic response of a semireverberant enclosure with application to active noise control
- Annualized TASAR benefit estimate for Alaska Airlines operations
- Annualized TASAR benefit estimate for Virgin America operations
- Application of CARS to scramjet combustion
- Application of SAE ARP4754A to flight critical systems
- Application of a Runge-Kutta scheme for high-speed inviscid internal flows
- Application of benchmark examples to assess the single and mixed-mode static delamination propagation capabilities in ANSYS®
- Application of decomposition techniques to the preliminary design of a transport aircraft
- Application of deterministic and probabilistic system design methods and enhancements of conceptual design tools for ERA project
- Application of strategic planning process with fleet level analysis methods : final report
- Application of the ASP3D computer program to unsteady aerodynamic and aeroelastic analyses
- Application of video image correlation techniques to the Space Shuttle External Tank foam materials
- Applications of fault detection in vibrating structures
- Applied operations research : augmented reality in an industrial environment
- Applied operations research : operator's assistant
- Applying pressure sensitive paint technology to rotor blades
- Approaches to control of the large angle magnetic suspension test fixture
- Approaches toward a blue semiconductor laser
- Approximate pressure distribution in an accelerating launch-vehicle fuel tank
- Architectural optimization of digital libraries
- Ares I-X flight test vehicle : stack 1 modal test
- Ares I-X flight test vehicle : stack 5 modal test
- Ares I-X flight test vehicle modal test
- Artificial boundary conditions for computation of oscillating external flows
- Artificial intelligence based control power optimization on tailless aircraft : ARMD seedling fund, phase I, final report
- Assembly and integration of superconductive measurement circuits for a spaceflight experiment
- Assess/mitigate risk through the use of computer-aided software engineering (CASE) tools
- Assessing V&V processes for automation with respect to vulnerabilities to loss of airplane state awareness
- Assessing the Amazon cloud suitability for CLARREO's computational needs
- Assessment of an explicit algebraic Reynolds stress model
- Assessment of microphone phased array for measuring launch vehicle lift-off acoustics
- Asteroid redirect mission (ARM) formulation assessment and support team (FAST) final report
- Asymptotic Waveform Evaluation (AWE) technique for frequency domain electromagnetic analysis
- Atmospheric ionizing radiation and human exposure
- Atmospheric solar absorption measurements in the 9 to 11 [mu]m region using a diode laser heterodyne spectrometer
- Autoclave processing for composite material fabrication. 1. An analysis of resin flows and fiber compactions for thin laminate
- Automated boundary conditions for wind tunnel simulations
- Automated verification of specifications with typestates and access permissions
- Autonomous flight rules : a concept for self-separation in U.S. domestic airspace
- Autonomous inspection of electrical transmission structures with airborne UV sensors : NASA report on Dominion Virginia Power flights of November 2016
- Autonomous path-following for a tilt-wing, distributed electric propulsion, vertical take-off and landing unmanned aerial system in hover mode
- Avionic pictorial tunnel-/pathway-/highway-in-the-sky workshops
- Avionics configuration assessment for flightdeck interval management : a comparison of avionics and notification methods
- Awareness and detection of traffic and obstacles using synthetic and enhanced vision systems
- Baseline assessment and prioritization framework for IVHM integrity assurance enabling capabilities
- Bayesian safety risk modeling of human-flightdeck automation interaction
- Bearing-load modeling and analysis study for mechanically connected structures
- Behind start of take-off roll aircraft sound level directivity study- revision 1 : final report
- Benefit assessment for metroplex tactical runway configuration management (mTRCM) in a simulated environment
- Bi-level integrated system synthesis (BLISS)
- Bi-metallic composite structures with designed internal residual stress field
- Big data analytics and machine intelligence capability development at NASA Langley Research Center : strategy, roadmap, and progress
- Binomial test method for determining probability of detection capability for fracture critical applications
- Blended wing body concept development with open rotor engine integration
- Boundary closures for fourth-order Energy Stable Weighted Essentially Non-Oscillatory finite difference schemes
- Boundary shape identification problems in two-dimensional domains related to thermal testing of materials
- Bowles-Tatnall wake vortex encounter hazard metric
- Breakdown characteristics of an isolated conducting object in a uniform electric field
- Broad band effective and affordable approaches to climate
- Broadband noise control using predictive techniques
- Bubble Memory Module
- Buckets, aggregative, intelligent agents for publishing
- Buckling analysis for stiffened anisotropic circular cylinders based on Sanders' nonlinear shell theory
- Buckling of thin-walled circular cylinders
- Buckling test results and preliminary test and analysis correlation from the 8-foot-diameter orthogrid-stiffened cylinder test article TA02 : test dates: 3-6 February 2009
- Buckling test results from the 8-foot-diameter orthogrid-stiffened cylinder test article TA01 : test dates: 19-21 November 2008
- Bunch-Kaufman factorization for real symmetric indefinite banded matrices
- CFD analysis of flexible thermal protection system shear configuration testing in the LCAT facility
- CFD study of NACA 0018 airfoil with flow control
- CFL3D contribution to the AIAA Supersonic Shock Boundary Layer Interaction Workshop
- COSAL : a black-box compressible stability analysis code for transition prediction in three-dimensional boundary layers
- COxSwAIN : compressive sensing for advanced imaging and navigation
- CWG, a FORTRAN program for mutual coupling in a planar array of circular waveguide-fed apertures
- Calculated low-speed steady and time-dependent aerodynamic derivatives for some airfoils using a discrete vortex method
- Calculation of laminar heating rates on three-dimensional configurations using the axisymmetric analogue
- Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment
- Calibration of a structural finite element model for a representative inflatable space structure utilizing probabilistic methods and surrogate models
- Calibration of sonic valves for the laminar flow control, leading-edge flight test
- Capture-ejector satellites
- Cavity heating experiments supporting Shuttle Columbia accident investigation
- Central Africa energy : utilizing NASA Earth observations to explore flared gas as an energy source alternative to biomass in Central Africa
- Characteristic vector analysis of inflection ratio spectra : new technique for analysis of ocean color data
- Characterization of Al-Cu-Li alloy 2090 near net shape extrusion
- Characterization of HIRF susceptibility threshold for a prototype implementation of an onboard data network
- Characterization of a 16-bit digitizer for lidar data acquisition
- Characterization of cavity flow fields using pressure data obtained in the Langley 0.3-meter transonic cryogenic tunnel
- Characterization of low frequency auditory filters
- Characterization of multilayer piezoelectric actuators for use in active isolation mounts
- Characterization of polymer-coated MEMS humidity sensors for flight applications
- Characterization of residual stress effects on fatigue crack growth of a friction stir welded aluminum alloy
- Characterization of the bending stiffness of large space structure joints
- Charge exchange transition probability for collisions between unlike ions and atoms within the adiabatic approximation
- Check-cases for verification of 6-degree-of-freedom flight vehicle simulations
- Chemical kinetic models for combustion of hydrocarbons and formation of nitric oxide
- Chemoviscosity modeling for thermosetting resins : final report for the period ended August 31, 1985
- Climate change and vector borne diseases on NASA Langley Research Center
- Coherent large-scale structures in high Reynolds number supersonic jets
- Collected papers in structural mechanics honoring Dr. James H. Starnes, Jr
- Colombia Mi Pronóstico flood application : updating and improving the Mi Pronóstico flood web application to include an assessment of flood risk
- Combined bearing and bypass loading on a graphite/epoxy laminate
- Combined load test fixture
- Combining through-thickness reinforcement and self-healing for improved damage tolerance and durability of composites
- Comments on the diffusive behavior of two upwind schemes
- Commercial cargo derivative study of the advanced hybrid wing body configuration with over-wing engine nacelles
- Comparative performance of HgCdTe photodiodes for heterodyne application
- Comparison of DAC and MONACO DSMC codes with flat plate simulation
- Comparison of NACA 0012 laminar flow solutions : structured and unstructured grid methods
- Comparison of Space Shuttle Orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests
- Comparison of Theodorsen's unsteady aerodynamic forces with double lattice generalized aerodynamic forces
- Comparison of analysis with test for static loading of two hypersonic inflatable aerodynamic decelerator concepts
- Comparison of effects of copropagated and precomputed atmosphere profiles on Monte Carlo trajectory simulation
- Comparison of flight simulators based on human motion perception metrics
- Comparison of requirements for composite structures for aircraft and space applications
- Comparison of separation shock for explosive and nonexplosive release actuators on a small spacecraft panel
- Comparison of the booster interface temperature in stainless steel (SS) v-channel versus the aluminum (Al) y-channel Primer Chamber Assemblies (PCAs)
- Comparisons of methods for predicting community annoyance due to sonic booms
- Compilation and review of supersonic business jet studies from 1963 through 1995
- Complex permittivities of candidate radome materials at W-band
- Composite Crew Module (CCM) permeability characterization
- Composite crew module : primary structure
- Composite interlaminar shear fracture toughness, G[sub IIc] : shear measurement or sheer myth?
- Composite stress rupture : a new reliability model based on strength decay
- Composite structures damage tolerance analysis methodologies
- Comprehensive lifecycle for assuring system safety
- Compressibility considerations for [kappa-omega] turbulence models in hypersonic boundary layer applications
- Compression after impact experiments and analysis on honeycomb core sandwich panels with thin facesheets
- Compression response of a sandwich fuselage keel panel with and without damage
- Compressive testing of stitched frame and stringer alternate configurations
- Computation of sound generated by viscous flow over a circular cylinder
- Computational performance of progressive damage analysis of composite laminates using Abaqus/Explicit with 16 to 512 CPU cores
- Compute as fast as the engineers can think! : ultrafast computing team final report
- Computed structures of polyimides model compounds
- Computer program for post-flight analysis of rigid body moments acting on a launch vehicle first stage
- Computer program for post-flight evaluation of a launch vehicle upper-stage on-off reaction control system
- Computer program for prediction of fuel consumption statistical data for an upper stage three-axes stabilized on-off control system
- Computer program to obtain ordinates for NACA airfoils
- Computer-Aided Design (CAD) tools to support the human factors design teams
- Computer-automated opponent for manned air-to-air combat simulations
- Concept development for software health management
- Concept of operations for integrating commercial supersonic transport aircraft into the National Airspace System
- Concept of operations for management by trajectory
- Concepts for conformal and body-axis attitude information for spatial awareness presented in a helmet-mounted display
- Conceptual design of a communications relay satellite for a Lunar sample return mission
- Conceptual design standards for eXternal Visibility System (XVS) sensor and display resolution
- Conceptual model of turbulent flameholding for scramjet combustors
- Conditions for symmetries in the buckle patterns of laminated-composite plates
- Conducting safe and efficient airport surface operations in a NextGen environment
- Configuration management of an optimization application in a research environment
- Conical shock-strength determination on low-sonic-boom aircraft model by doppler global velocimetry
- Connective heating improvement for emergency fire shelters : composition and performance of fire shelter concepts at close-out
- Conservative finite volume solutions of a linear hyperbolic transport equation in two and three dimensions using multiple grids
- Consideration of some factors affecting low-frequency fuselage noise transmission for propeller aircraft
- Considering risk and resil