Книги з теми "Inlet distortions"

A, Ladd J., Yuhas A. J, and United States. National Aeronautics and Space Administration., eds. Dynamic inlet distortion prediction with a combined computational fluid dynamics and distortion synthesis approach. [Washington, DC: National Aeronautics and Space Administration, 1996.

M, Greitzer Edward, and Lewis Research Center, eds. Final technical report on grant NAG3-1567 entitled Inlet distortion in engines on VSTOL aircraft. Cleveland, OH: The Center, 1994.

Yuhas, Andrew J. Design and development of an F/A-18 inlet distortion rake: a cost and time saving solution. Edwards, Calif: Dryden Flight Research Center, 1995.

United States. Army Aviation Research and Technology Activity. and United States. National Aeronautics and Space Administration., eds. Effects of inlet distortion on the development of secondary flows in a subsonic axial inlet compressor rotor. [Washington, DC]: National Aeronautics and Space Administration, 1991.

H, Anderson Bernhard, Shaw Robert J. 1946-, and United States. National Aeronautics and Space Administration., eds. A full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application. [Washington, DC]: National Aeronautics and Space Administration, 1994.

H, Anderson Bernhard, Shaw Robert J. 1946-, and United States. National Aeronautics and Space Administration., eds. A full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application. [Washington, DC]: National Aeronautics and Space Administration, 1994.

D, Baust Henry, Agrell Johan, and NASA Glenn Research Center, eds. Management of total pressure recovery, distortion and high cycle fatigue in compact air vehicle inlets. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2002.

H, Anderson Bernhard, and United States. National Aeronautics and Space Administration., eds. A study on vortex flow control on inlet distortion in the re-engined 727-100 center inlet duct using computational fluid dynamics. [Washington, DC]: National Aeronautics and Space Administration, 1992.

1945-, Levy R., and United States. National Aeronautics and Space Administration., eds. A design strategy for the use of vortex generators to manage inlet-engine distortion using computational fluid dynamics. [Washington, DC]: National Aeronautics and Space Administration, 1991.

Center, Ames Research, ed. Sea level static calibration of a compact multimission aircraft propulsion simulator with inlet flow distortion. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1991.

G, Williams J. Estimating engine airflow in gas-turbine powered aircraft with clean and distorted inlet flows. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1996.

Podleski, Steve D. PARC3D calculations of the F/A-18A HARV inlet vortex generators. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

M, Mehalic Charles, Stancik Kevin, and Lewis Research Center, eds. Effect of steady-state temperature distortion on inlet flow to a high-bypass-ratio turbofan engine. Cleveland, Ohio: Lewis Research Center, 1985.

M, Mehalic Charles, Stancik Kevin, and Lewis Research Center, eds. Effect of steady-state temperature distortion on inlet flow to a high-bypass-ratio turbofan engine. Cleveland, Ohio: Lewis Research Center, 1985.

M, Mehalic Charles, Stancik Kevin, and Lewis Research Center, eds. Effect of steady-state temperature distortion on inlet flow to a high-bypass-ratio turbofan engine. Cleveland, Ohio: Lewis Research Center, 1985.

M, Mehalic Charles, Stancik Kevin, and Lewis Research Center, eds. Effect of steady-state temperature distortion on inlet flow to a high-bypass-ratio turbofan engine. Cleveland, Ohio: Lewis Research Center, 1985.

M, Mehalic Charles, Stancik Kevin, and Lewis Research Center, eds. Effect of steady-state temperature distortion on inlet flow to a high-bypass-ratio turbofan engine. Cleveland, Ohio: Lewis Research Center, 1985.

Steenken, William G. An inlet distortion assessment during aircraft departures at high angle of attack for an F/A-18A aircraft. Edwards, Calif: NASA Dryden Flight Research Center, 1997.

James, Gibb, and United States. National Aeronautics and Space Administration., eds. Application of computational fluid dynamics to the study of vortex flow control for the management of inlet distortion. [Washington, DC: National Aeronautics and Space Administration, 1992.

NASA Dryden Flight Research Center., ed. An inlet distortion assessment during aircraft departures at high angle of attack for an F/A-18A aircraft. Edwards, Calif: NASA Dryden Flight Research Center, 1997.

P, Myers Lawrence, Mackall Karen G, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Effects of inlet distortion on a static pressure probe mounted on the engine hub in an F-15 airplane. Washington, D.C: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

R, Walsh Kevin, and NASA Dryden Flight Research Center., eds. Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ̊angle of attack: Contract NAS 3-26617. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1997.

R, Walsh Kevin, and NASA Dryden Flight Research Center., eds. Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ̊angle of attack: Contract NAS 3-26617. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1997.

Inlet Distortion Generation for a Transonic Compressor. Storming Media, 2004.

Circumferential Distortion of the Inlet Flow in an Axial Compressor. Creative Media Partners, LLC, 2021.

Comparison of Predicted and Measured Inlet Distortion Flows in a Subsonic Axial Inlet Flow Compressor Rotor. Independently Published, 2020.

National Aeronautics and Space Administration (NASA) Staff. Analysis of Dynamic Inlet Distortion Applied to a Parallel Compressor Model. Independently Published, 2018.

Effect of spatial inlet temperature and pressure distortion on turbofan engine stability. [Washington, DC]: National Aeronautics and Space Administration, 1988.

A full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application. [Washington, DC]: National Aeronautics and Space Administration, 1994.

A full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application. [Washington, DC]: National Aeronautics and Space Administration, 1994.

Ultra high bypass nacelle areodynamics: Inlet flow-through high angle of attack distortion test. [Washington, DC: National Aeronautics and Space Administration, 1992.

National Aeronautics and Space Administration (NASA) Staff. Ultra High Bypass Nacelle Aerodynamics Inlet Flow-Through High Angle of Attack Distortion Test. Independently Published, 2018.

Engine inlet distortion in a 9.2 percent scale vectored thrust STOVL model in ground effect. [Washington, DC: National Aeronautics and Space Administration, 1990.

Theoretical and experimental study of flow-control devices for inlets of indraft wind tunnels. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.

Theoretical and experimental study of flow-control devices for inlets of indraft wind tunnels. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.

Effect of steady-state temperature distortion on inlet flow to a high-bypass-ratio turbofan engine. Cleveland, Ohio: Lewis Research Center, 1985.