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Results for “COMPRESSORS - BLADES”

Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.

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At least 397 records · Page 22

All sources NASA NTRS DOE OSTI

NASA NTRS1970

XB-70 compressor-noise reduction and propulsion-system performance for choked inlet flow

XB-70 compressor noise reduction and propulsion system performance for choked inlet flow

Putnam, T. W.↗

NASA NTRS1969

Measurements of the Van der Waals Na - lambda 5889 in He with a newly developed piston compressor light source

Measurements of Van der Waals Na 5889 A in He with piston compressor light source

Grindlay, J. E.↗

NASA NTRS1969

Design and development of a resonant piston compressor for hermetically sealed platforms

Resonant piston compressor for recirculation system of hermetically sealed platform

Curwen, P. W.↗

NASA NTRS1970

Experimental evaluation of outer case blowing or bleeding of single stage axial flow compressor, part 6 Final report

Evaluation of outer case blowing or bleeding of single stage axial flow compressor

Koch, C. C.↗

NASA NTRS1970

The effect of inlet temperature distortion on the performance of a turbo-fan engine compressor system

Inlet temperature distortion effect on performance of turbofan engine compressor systems

Antl, R. J.↗

NASA NTRS1970

Dynamic analysis of XB-70-1 inlet pressure fluctuations during takeoff and prior to a compressor stall at Mach 2.5

Inlet pressure fluctuation in XB-70 aircraft during takeoff and prior to compressor stall at Mach 2.5

Martin, R. A.↗

NASA NTRS1970

Single-stage evaluation of highly-loaded high- Mach-number compressor stages. 2 - Data and performance, multiple-circular-arc rotor

Single stage evaluation of highly loaded high Mach number compressor stages - data and performance multiple circular arc rotor

Flynn, J. T.↗

NASA NTRS1970

Compressor end seal test and development

Design and test of hydrostatic compressor end seals

Moore, C. C.↗

NASA NTRS1970

Effect of dynamic variations in engine-inlet pressure on the compressor system of a twin- spool turbofan engine

Inlet pressure oscillation effects on turbofan engine compressor

Mc Aulay, J. E.↗

NASA NTRS1970

Theoretical analysis of compressor noise

Far field directionality and acoustic power of noise radiated by axial flow fans and compressors using fluctuating forces model

Lowson, M. V.↗

NASA NTRS1970

Analysis of in-flight pressure fluctuations leading to engine compressor surge in an F-111A airplane for Mach numbers to 2.17

F-111A airplane in-flight inlet pressure fluctuations for engine compressor surge, discussing average turbulence factor

Burcham, F. W., Jr.↗

NASA NTRS1970

The effect of inlet temperature distortion on the performance of a turbo-fan engine compressor system

Turbofan engine compressor system performance dependence on circumferential extent, magnitude and rate of change of inlet temperature in altitude test facility

Antl, R. J.↗

NASA NTRS1970