Turbocompressors

32 books
Design of 9.271-pressure-ratio five-stage core compressor and overall performance for first three stagesRonald J. Steinke
⏱ 32m

Design of 9.271-pressure-ratio five-stage core compressor and overall performance for first three stages

Ronald J. Steinke

198632 pp.
Axial-flow compressor noise (generation, transmission and radiation of discrete frequency components)Shojiro Kaji

Axial-flow compressor noise (generation, transmission and radiation of discrete frequency components)

Shojiro Kaji

No page data
NASA low-speed axial compressor for fundamental researchCharles A. Wasserbauer
⏱ 11m

NASA low-speed axial compressor for fundamental research

Charles A. Wasserbauer

199511 pp.
Application of modified loss and deviation correlations to transonic axial compressorsM. Cetin
⏱ 1h 4m

Application of modified loss and deviation correlations to transonic axial compressors

M. Cetin

198764 pp.
Aerodynamic broadband noise mechanisms applicable to axial compressorsRobert A. Arnoldi
⏱ 38m

Aerodynamic broadband noise mechanisms applicable to axial compressors

Robert A. Arnoldi

197038 pp.
Demonstration of PIV in a transonic compressorMark P. Wernet

Demonstration of PIV in a transonic compressor

Mark P. Wernet

1997No page data
Off-design computer code for calculating the aerodynamic performance of axial-flow fans and compressorsJames F. Schmidt

Off-design computer code for calculating the aerodynamic performance of axial-flow fans and compressors

James F. Schmidt

1995No page data
Blading design for axial turbomachinesNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.

Blading design for axial turbomachines

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.

1989No page data
Small engine technologyJeff L. Hansen

Small engine technology

Jeff L. Hansen

1997No page data
Effects of stator indexing on performance in a low speed multistage axial compressorWendy S. Barankiewicz

Effects of stator indexing on performance in a low speed multistage axial compressor

Wendy S. Barankiewicz

1997No page data
Inlet flow test calibration for a small axial compressor facilityD. P. Miller

Inlet flow test calibration for a small axial compressor facility

D. P. Miller

1994No page data
Dimension determination of precursive stall events in a single stage high speed compressorMichelle M. Bright

Dimension determination of precursive stall events in a single stage high speed compressor

Michelle M. Bright

1996No page data
Enhanced capabilities and modified users manual for axial-flow compressor conceptual design code CSPANArthur J. Glassman

Enhanced capabilities and modified users manual for axial-flow compressor conceptual design code CSPAN

Arthur J. Glassman

1995No page data
A final report on NASA grant NGL-22-009-383 entitled Unsteady design-point flow phenomena in transonic compressorsJ. R. Gertz

A final report on NASA grant NGL-22-009-383 entitled Unsteady design-point flow phenomena in transonic compressors

J. R. Gertz

1986No page data
Rotordynamics and design methods of an oil-free turbochargerSamuel A. Howard

Rotordynamics and design methods of an oil-free turbocharger

Samuel A. Howard

1999No page data
Effects of shrouded stator cavity flows on multistage axial compressor aerodynamic performanceSteven R. Wellborn

Effects of shrouded stator cavity flows on multistage axial compressor aerodynamic performance

Steven R. Wellborn

1996No page data
Secondary flow spanwise deviation model for the stators of NASA middle compressor stagesWilliam B. Roberts

Secondary flow spanwise deviation model for the stators of NASA middle compressor stages

William B. Roberts

1984No page data
Static flow characteristics of a mass flow injecting valveDuane L. Mattern

Static flow characteristics of a mass flow injecting valve

Duane L. Mattern

1995No page data
WINCLRBose, T. K.

WINCLR

Bose, T. K.

1994No page data
The effect of adding roughness and thickness to a transonic axial compressor rotorUnknown Author

The effect of adding roughness and thickness to a transonic axial compressor rotor

Unknown Author

1995No page data
Page 1 of 2Next →