Aerodynamics
Resource Information
The concept Aerodynamics represents the subject, aboutness, idea or notion of resources found in San Francisco Public Library.
The Resource
Aerodynamics
Resource Information
The concept Aerodynamics represents the subject, aboutness, idea or notion of resources found in San Francisco Public Library.
- Label
- Aerodynamics
- Source
- nasat
54 Items that share the Concept Aerodynamics
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- Variable-speed power-turbine research at Glenn Research Center
- A parametric study of accelerations of an airplane due to a wake vortex system
- A survey of challenges in aerodynamic exhaust nozzle technology for aerospace propulsion applications
- AMT-200S motor glider parameter and performance estimation
- Aerodynamic design of a propeller for high-altitude balloon trajectory control
- Aerodynamics of a transitioning turbine stator over a range of Reynolds numbers
- An experimental evaluation of the performance of two combination pitot pressure probes
- An overview of the NASA F-18 high alpha research vehicle
- An overview of three approaches to multidisciplinary aeropropulsion simulations
- Application of approximate unsteady aerodynamics for flutter analysis
- Assessment of aerodynamic challenges of a variable-speed power turbine for large civil tilt-rotor application
- Autonomous momentum management for space station : final report, 15 October 1984
- Computational fluid dynamics (CFD) simulation of hypersonic turbine-based combined-cycle (TBCC) inlet mode transition
- Control activity in support of NASA Turbine Based Combined Cycle (TBCC) research
- Design guide for aerodynamics testing of Earth and planetary entry vehicles in a ballistic range
- Design of a slotted, natural-laminar-flow airfoil for business-jet applications
- Design-of-experiments to reduce life-cycle costs in combat aircraft inlets
- Development of an open rotor cycle model in NPSS using a multi-design point approach
- Development of experimental icing simulation capability for full-scale swept wings : hybrid design process, years 1 and 2
- Development of the Transport Class Model (TCM) aircraft simulation from a sub-scale Generic Transport Model (GTM) simulation
- Dynamic modeling of starting aerodynamics and stage matching in an axi-centrifugal compressor
- Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV
- Enhancement/upgrade of Engine Structures Technology Best Estimator (EST/BEST) software system
- Experimental performance and analysis of 15.04-centimeter-tip-diameter, radial-inflow turbine with work factor of 1.126 and thick blading
- Finite element modeling and analysis of Mars entry aeroshell concept
- Fluid physics
- Further evaluation of scaling methods for rotorcraft icing
- Guide to AERO2S and WINGDES computer codes for prediction and minimization of drag due to lift
- High fidelity CFD analysis and validation of rotorcraft gearbox aerodynamics under operational and oil-out conditions : final report
- Ice accretions and full-scale iced aerodynamic performance data for a two-dimensional NACA 23012 airfoil
- Integration of a CAD system into an MDO framework
- Introduction of the ASP3D computer program for unsteady aerodynamic and aeroelastic analyses
- Missile aerodynamics for ascent and re-entry
- Multi-objective optimization of a turbofan for an advanced, single-aisle transport
- Nonlinear aerodynamic modeling from flight data using advanced piloted maneuvers and fuzzy logic
- Numerical study of three-dimensional separation and flow control at a wing-body junction : progress report for the period ended April 30, 1989
- Optimal regulation in systems with stochastic time sampling
- PLTTER user's guide
- Preliminary sizing of vertical take-off rocket-based combined-cycle powered launch vehicles
- Research opportunities in advanced aerospace concepts
- Review of research on angle-of-attack indicator effectiveness
- Rotary-wing relevant compressor aero research and technology development activities at Glenn Research Center
- Rotating rig development for droplet deformation/breakup and impact induced by aerodynamic surfaces
- Sensor-only system identification for structural health monitoring of advanced aircraft
- Subsonic dynamics of stardust sample return capsule
- Swept-wing ice accretion characterization and aerodynamics
- Tabulation of data from the tip aerodynamics and acoustics test
- The effects of Reynolds number, rotor incidence angle and surface roughness on the heat transfer distribution in a large-scale turbine rotor passage
- The effects of inlet turbulence and rotor/stator interactions on the aerodynamics and heat transfer of a large-scale rotating turbine model : IV--aerodynamic data tabulation
- Turbulence intensity at inlet of 80- by 120-foot wind tunnel caused by upwind blockage
- Unsteady aero computation of a 1 1/2 stage large scale rotating turbine
- VORCOR : a computer program for calculating characteristics of wings with edge vortex separation by using a vortex filament and core model
- Validation of design and analysis techniques of tailored composite structures
- Variable-speed power-turbine for the large civil tilt rotor
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.sfpl.org/resource/2eDgaRN-jpM/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.sfpl.org/resource/2eDgaRN-jpM/">Aerodynamics</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.sfpl.org/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="https://link.sfpl.org/">San Francisco Public Library</a></span></span></span></span></div>
