Książki na temat „Inlet distortions”

A, Ladd J., Yuhas A. J i United States. National Aeronautics and Space Administration., red. 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, i Lewis Research Center, red. 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. i United States. National Aeronautics and Space Administration., red. 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- i United States. National Aeronautics and Space Administration., red. 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- i United States. National Aeronautics and Space Administration., red. 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 i NASA Glenn Research Center, red. 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, i United States. National Aeronautics and Space Administration., red. 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., i United States. National Aeronautics and Space Administration., red. 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, red. 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 i Lewis Research Center, red. 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 i Lewis Research Center, red. 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 i Lewis Research Center, red. 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 i Lewis Research Center, red. 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 i Lewis Research Center, red. 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, i United States. National Aeronautics and Space Administration., red. 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., red. 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 i United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., red. 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, i NASA Dryden Flight Research Center., red. 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, i NASA Dryden Flight Research Center., red. 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.