Books on the topic 'Compression flows'

H, Anderson Bernhard, Shaw Robert J. 1946-, and United States. National Aeronautics and Space Administration., eds. Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code. [Washington, DC]: National Aeronautics and Space Administration, 1994.

Center, Ames Research, ed. Steady secondary flows generated by periodic compression and expansion of an ideal gas in a pulse tube. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1999.

B, Roebuck, and National Physical Laboratory (Great Britain), eds. Measuring flow stress in hot axisymmetric compression tests. Teddington: NPL, 1997.

Neuhoff, F. Modifications to the inlet flow field of a transonic compressor rotor. Monterey, Calif: Naval Postgraduate School, 1985.

Stalker, R. J. Thermodynamics and wave processes in high Mach number propulsive ducts. Washington: AIAA, 1989.

1936-, Kawamura Takaichi, Bencze Daniel P, and Ames Research Center, eds. Calculation of external-internal flow fields for mixed-compression inlets. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

1936-, Kawamura Takaichi, Bencze Daniel P, and Ames Research Center, eds. Calculation of external-internal flow fields for mixed-compression inlets. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

Center, Ames Research, ed. Computations of unsteady multistage compressor flows in a workstation environment. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1992.

S, Prahst P., and United States. National Aeronautics and Space Administration., eds. Inlet flow test calibration for a small axial compressor facility. [Washington, DC]: National Aeronautics and Space Administration, 1994.

United States. National Aeronautics and Space Administration., ed. Blockage development in a transonic, axial compressor rotor. [Washington, D.C: National Aeronautics and Space Administration, 1997.

United States. National Aeronautics and Space Administration., ed. Blockage development in a transonic, axial compressor rotor. [Washington, D.C: National Aeronautics and Space Administration, 1997.

Ng, Y. K. Eddie. Compressor instability with integral methods. Berlin: Springer, 2007.

Maurice, M. S. The LV measured turbulent structure of Mach 6 flow over a roughened flat plate with a compression ramp. New York: AIAA, 1989.

C, Bidek Maleina, and United States. National Aeronautics and Space Administration., eds. Turbulence models and Reynolds analogy for two-dimensional supersonic compression ramp flow. [Washington, DC: National Aeronautics and Space Administration, 1994.

1939-, Okiishi T. H., and United States. National Aeronautics and Space Administration., eds. Effects of shrouded stator cavity flows on multistage axial compressor aerodynamic performance. [Washington, DC]: National Aeronautics and Space Administration, 1996.

Cherrett, M. A. Unsteady viscous flow in a high speed core compressor. Farnborough, Hampshire: Procurement Executive, Ministry of Defence, 1990.

Li, Ruiyu, Limin Gao, and Lei Zhao. Detached-Eddy Simulation Series Methods for Compressor Internal Flow. Singapore: Springer Nature Singapore, 2025. https://doi.org/10.1007/978-981-96-0255-1.

McKenzie, A. B. Axial compressor development at Rolls-Royce Derby, 1946-1962. Derby: Rolls-Royce Heritage Trust, 2009.

Center, NASA Glenn Research, ed. On hammershock propagation in a supersonic flow field. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2002.

D, Saunders J., and United States. National Aeronautics and Space Administration., eds. 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet. [Washington, DC]: National Aeronautics and Space Administration, 1995.

D, Saunders J., and United States. National Aeronautics and Space Administration., eds. 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet. [Washington, DC]: National Aeronautics and Space Administration, 1995.

D, Saunders J., and United States. National Aeronautics and Space Administration., eds. 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet. [Washington, DC]: National Aeronautics and Space Administration, 1995.

D, Saunders J., and United States. National Aeronautics and Space Administration., eds. 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet. [Washington, DC]: National Aeronautics and Space Administration, 1995.

S, Prahst P., and United States. National Aeronautics and Space Administration., eds. Inlet flow test calibration for a small axial compressor rig. [Washington, DC]: National Aeronautics and Space Administration, 1995.

Perttula, Juha. Physical simulation of hot working: Measurements of flow stress and recrystallization kinetics. Oulu: Oulun yliopisto, 1998.

D, Saunders J., and United States. National Aeronautics and Space Administration., eds. Parametrics on 2D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet. [Washington, DC]: National Aeronautics and Space Administration, 1995.

D, Saunders J., and United States. National Aeronautics and Space Administration., eds. Parametrics on 2D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet. [Washington, DC]: National Aeronautics and Space Administration, 1995.

United States. National Aeronautics and Space Administration., ed. A final report on NASA grant NGL-22-009-383 entitled Unsteady design-point flow phenomena in transonic compressors: Final report. Cambridge, MA: Gas Turbine Laboratory, Dept. of Aeronautics and Astronautics, Massachusetts Institute of Technology, 1986.

Haynes, Joel M. Active control of rotating stall in a three-stage axial compressor. Cambridge, Mass: Gas Turbine Laboratory, Massachusetts Institute of Technology, 1993.

Hathaway, Michael D. Self-recirculating casing treatment concept for enhanced compressor performance. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2002.

Center, NASA Glenn Research, ed. Self-recirculating casing treatment concept for enhanced compressor performance. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2002.

Center, NASA Glenn Research, ed. Self-recirculating casing treatment concept for enhanced compressor performance. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2002.

Center, NASA Glenn Research, ed. Self-recirculating casing treatment concept for enhanced compressor performance. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2002.

United States. National Aeronautics and Space Administration., ed. Users manual for updated computer code for axial-flow compressor conceptual design. [Washington, DC: National Aeronautics and Space Administration, 1992.

F, Weaver Harold, Senyitko Richard G, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. NASA low-speed axial compressor for fundamental research. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.

F, Weaver Harold, Senyitko Richard G, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. NASA low-speed axial compressor for fundamental research. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.

F, Weaver Harold, Senyitko Richard G, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. NASA low-speed axial compressor for fundamental research. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.

Wasserbauer, Charles A. NASA low-speed axial compressor for fundamental research. Cleveland, Ohio: Lewis Research Center, 1995.

F, Weaver Harold, Senyitko Richard G, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. NASA low-speed axial compressor for fundamental research. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.

L, Gundy-Burlet Karen, and Ames Research Center, eds. Temporally and spatially resolved flow in a two-stage axial compressor. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.

L, Gundy-Burlet Karen, and Ames Research Center, eds. Temporally and spatially resolved flow in a two-stage axial compressor. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.

W, Tam C. K., and United States. National Aeronautics and Space Administration., eds. Numerical simulation of the generation of axisymmetric mode jet screech tones. Reston, Va: American Institute of Aeronautics and Astronautics, 1998.

W, Tam C. K., and United States. National Aeronautics and Space Administration., eds. Numerical simulation of the generation of axisymmetric mode jet screech tones. Reston, Va: American Institute of Aeronautics and Astronautics, 1998.

Moore, John. A prediction of 3-D viscous flow and performance of the NASA low-speed centrifugal compressor. Blacksburg, Va: Mechanical Engineering Dept., Virginia Polytechnic Institute and State University, 1989.

Moore, John. A prediction of 3-D viscous flow and performance of the NASA low-speed centrifugal compressor. Blacksburg, Va: Mechanical Engineering Dept., Virginia Polytechnic Institute and State University, 1989.

C, Smith Steven. Airflow calibration of a bellmouth inlet for measurement of compressor airflow in turbine-powered propulsion simulators. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1985.

Cuellar, Alvaro F. Measurement of synchronous forces and flow non-uniformity in an axial compressor. Monterey, Calif: Naval Postgraduate School, 1997.

United States. National Aeronautics and Space Administration., ed. Experimental determination of aerodynamic damping in a three-syage transonic axial-flow compressor. [Washington, DC: National Aeronautics and Space Administration, 1988.

Chung-hua, Wu. A general theory of two-and three-dimensional rotational flow in subsonic and transonic turbomachines. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

Chung-hua, Wu. A general theory of two-and three-dimensional rotational flow in subsonic and transonic turbomachines. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.