Книги з теми "Mixed Compression"

Oppitz, Rick. Aerothermodynamic performance of mixed compression, shock-induced combustion ramjets. [Downsview, Ont.]: University of Toronto, Institute for Aerospace Studies, 1995.

Oppitz, Richard Andrew. Aerothermodynamic performance of mixed compression, shock-induced combustion ramjets. Ottawa: National Library of Canada, 1995.

Fisher, S. A. Internal performance of a variable ramp mixed compression intake at Mach 3.05. Melbourne, Vic: Aeronautical Research Laboratories, 1985.

Trefny, Charles J. Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets. Cleveland, Ohio: Lewis Research Center, 1986.

Redford, Tim. Effects of incomplete fuel-air mixing on the performance characteristics of mixed compression, shock-induced combustion ramjet (shcramjet) engines. Toronto]: Dept. of Aerospace Science and Engineering, University of Toronto, 1998.

Redford, Tim. Effects of incomplete fuel-air mixing on the performance characteristics of mixed compression, shock-induced combustion ramjet (shcramjet) engines. Ottawa: National Library of Canada, 1998.

Yunho, Hwang, ed. Vapor compression heat pumps with refrigerant mixes. Boca Raton, FL: Taylor & Francis, 2005.

Heredia Conde, Miguel. Compressive Sensing for the Photonic Mixer Device. Wiesbaden: Springer Fachmedien Wiesbaden, 2017. http://dx.doi.org/10.1007/978-3-658-18057-7.

Pavlidis, George. Mixed Raster Content: Segmentation, Compression, Transmission. Springer, 2016.

Pavlidis, George. Mixed Raster Content: Segmentation, Compression, Transmission. Springer, 2016.

Pavlidis, George. Mixed Raster Content: Segmentation, Compression, Transmission. Springer, 2018.

Alexander, Derrick. Hypersonic mixed-compression inlet shock-induced combustion ramjets. 2006.

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.

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.

G, Keith Theodore, and United States. National Aeronautics and Space Administration., eds. Results from computational analysis of a mixed compression supersonic inlet. Washington, DC: National Aeronautics and Space Administration, 1991.

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.

W, Wasserbauer Joseph, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

W, Wasserbauer Joseph, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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

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

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.

E, Neumann Harvey, Shaw Robert J. 1946-, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Performance and surge limits of a TF30-P-3 turbofan engine/axisymmetric mixed-compression inlet propulsion system at Mach 2.5. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

K, Bogue Rodney, Seidel Jonathan, and Hugh L. Dryden Flight Research Center., eds. The use of a lidar forward-looking turbulence sensor for mixed-compression inlet unstart avoidance and gross weight reduction on a high speed civil transport. [Edwards, Calif.]: National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.

Nyquist, Nathan. Mastering Multi-Band Compression: 17 Step by Step Multiband Compression Techniques for Getting Flawless Mixes. Independently Published, 2018.

Conde, Miguel Heredia. Compressive Sensing for the Photonic Mixer Device: Fundamentals, Methods and Results. Springer Fachmedien Wiesbaden GmbH, 2017.

Sanford, Fleeter, and United States. National Aeronautics and Space Administration, eds. The effect of prewhirl on the internal aerodynamics and performance of a mixed flow research centrifugal compressor. West Lafayette, Ind: Thermal Sciences and Propulsion Center, School of Mechanical Engineering, Purdue University, 1987.

Harkins, Hugh. Soviet Mixed Power Experimental Fighter Aircraft: Piston-Liquid Propellant Rocket Engine/Piston-Ramjet/Piston-Pulsejet & Piston-Compressor Jet Engine designs of the 1940’s. Centurion Publishing, 2018.