Pressure Ratio

18 books
Coordinates for a high performance 4:1 pressure ratio centrifugal compressorTed F. McKain

Coordinates for a high performance 4:1 pressure ratio centrifugal compressor

Ted F. McKain

1997No page data
Small engine technologyJeff L. Hansen

Small engine technology

Jeff L. Hansen

1997No page data
Effects of nozzle exit geometry and pressure ratio on plume shape for nozzles exhausting into quiescent airW. I. Scallion

Effects of nozzle exit geometry and pressure ratio on plume shape for nozzles exhausting into quiescent air

W. I. Scallion

1991No page data
Effect of area ratio on the performance of a 5.5:1 pressure ratio centrifugal impellerLawrence F. Schumann

Effect of area ratio on the performance of a 5.5:1 pressure ratio centrifugal impeller

Lawrence F. Schumann

1986No page data
Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65 ̊delta wings varying in leading-edge radius and camberUnknown Author

Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65 ̊delta wings varying in leading-edge radius and camber

Unknown Author

1996No page data
Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65 ̊delta wings varying in leading-edge radius and camberUnknown Author

Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65 ̊delta wings varying in leading-edge radius and camber

Unknown Author

1996No page data
Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65 ̊delta wings varying in leading-edge radius and camberUnknown Author

Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65 ̊delta wings varying in leading-edge radius and camber

Unknown Author

1996No page data
A performance map for ideal air breathing pulse detonation enginesDaniel E. Paxon

A performance map for ideal air breathing pulse detonation engines

Daniel E. Paxon

2001No page data
Analysis of a rocket based combined cycle engine during rocket only operationUnknown Author

Analysis of a rocket based combined cycle engine during rocket only operation

Unknown Author

1998No page data
Cellular structures in the flow over the flap of a two-element wingSteven A. Yon

Cellular structures in the flow over the flap of a two-element wing

Steven A. Yon

1997No page data
Static and wind tunnel aero-performance tests of NASA AST separate flow nozzle noise reduction configurationsKevin L. Mikkelsen

Static and wind tunnel aero-performance tests of NASA AST separate flow nozzle noise reduction configurations

Kevin L. Mikkelsen

2001No page data
High speed nozzles taskA. Hamed

High speed nozzles task

A. Hamed

1995No page data
A comparison of signal enhancement methods for extracting tonal acoustic signalsMichael G. Jones

A comparison of signal enhancement methods for extracting tonal acoustic signals

Michael G. Jones

1998No page data
Static internal performance of a two-dimensional convergent-divergent nozzle with external shelfMilton Lamb

Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf

Milton Lamb

1996No page data
Computational noise study of a supersonic short conical plug-nozzle jetIndu S. Das

Computational noise study of a supersonic short conical plug-nozzle jet

Indu S. Das

1996No page data
The noise reduction potential of dual-stream coaxial rectangular improperly expanded jet flowsDarshan Dosanjh

The noise reduction potential of dual-stream coaxial rectangular improperly expanded jet flows

Darshan Dosanjh

1995No page data
Calibration of sonic valves for the laminar flow control, leading-edge flight testUnknown Author

Calibration of sonic valves for the laminar flow control, leading-edge flight test

Unknown Author

1985No page data
An Introduction to Chemical Crystallography...Andreas Ludwig Fock
⏱ 4h 49m

An Introduction to Chemical Crystallography...

Andreas Ludwig Fock

1895289 pp.