Pressure distribution
Resource Information
The concept Pressure distribution represents the subject, aboutness, idea or notion of resources found in San Francisco Public Library.
The Resource
Pressure distribution
Resource Information
The concept Pressure distribution represents the subject, aboutness, idea or notion of resources found in San Francisco Public Library.
- Label
- Pressure distribution
- Source
- nasat
46 Items that share the Concept Pressure distribution
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- Wing leading edge joint laminar flow tests
- A comparison of pressure measurements between a full-scale and a 1/6-scale F/A-18 twin tail during buffet
- A non-cut cell immersed boundary method for use in icing simulations
- A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92
- Aerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade
- An airfoil flutter model suspension system to accomdate large static transonic airloads
- Approximate pressure distribution in an accelerating launch-vehicle fuel tank
- Background pressure profiles for sonic boom vehicle testing in the NASA Glenn 8- by 6-foot supersonic wind tunnel
- Base passive porosity for drag reduction
- Bidirectional brush seals : post-test analysis
- Characterization of cavity flow fields using pressure data obtained in the Langley 0.3-meter transonic cryogenic tunnel
- Contraction design for small low-speed wind tunnels
- Cure cycle design methodology for fabricating reactive resin matrix fiber reinforced composites : a protocol for producing void-free quality laminates
- DBD plasma actuators for flow control in air vehicles and jet engines : simulation of flight conditions in test chambers by density matching
- DBD plasma actuators for flow control in air vehicles and jet engines : simulation of flight conditions in test chambers by density matching
- Design and use of a guided weight impactor to impart barely visible impact damage
- Design concepts for cooled ceramic composite turbine vane
- Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV
- Effect of sweep on cavity flow fields at subsonic and transonic speeds
- Effects of velocity profile and inclination on dual-jet-induced pressures on a flat plate in a crosswind
- Exhaust plume effects on sonic boom for a delta wing and a swept wing-body model
- Experimental effects of wing location on wing-body pressures at supersonic speeds
- Experimental investigation of unsteady flows at large incidence angles in a linear oscillating cascade
- F-15B/flight test fixture II : a test bed for flight research
- Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing
- In-flight boundary-layer transition on a large flat plate at supersonic speeds
- Interaction of two-dimensional transverse jet with a supersonic mainstream
- Large eddy simulation of transonic flow field in NASA rotor 37
- Measured pressure distributions inside nonaxisymmetric nozzles with partially deployed thrust reversers
- Mir cooperative solar array flight performance data and computational analysis
- Onset of condensation effects with an NACA 0012-64 airfoil tested in the Langley 0.3-meter transonic cryogenic tunnel
- Prediction of sound fields in acoustical cavities using the boundary element method
- Pressure distribution for the wing of the YAV-8B airplane : with and without pylons
- Prevention of over-pressurization during combustion in a sealed chamber
- Reliability of COPVs accounting for margin of safety on design burst
- Results of design studies and wind tunnel tests of an advanced high lift system for an energy efficient transport
- Simulation of turbine tone noise generation using a turbomachinery aerodynamics solver
- Structural analysis and optimization of a composite fan blade for future aircraft engine
- Summary of pressure gain combustion research at NASA
- Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system
- The fast scattering code (FSC) : validation studies and program guidelines
- Three-dimensional flow field measurements in a transonic turbine cascade
- USSAERO version D computer program development using ANSI standard FORTRAN 77 and DI-3000 graphics
- Validation of a CFD methodology for variable speed power turbine relevant conditions
- Wind tunnel measured effects on a twin-engine short-haul transport caused by simulated ice accretions : data report
- Wind tunnel results of the aerodynamic performance of a 1/8-scale model of a twin-engine transport with multi-element wing
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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/tB85Ko_K8D8/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.sfpl.org/resource/tB85Ko_K8D8/">Pressure distribution</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>
