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Results for “compressors”

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 721 records · Page 40

All sources NASA NTRS DOE OSTI

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

Flow through cascades of slotted compressor blades

Incompressible two dimensional potential flow analysis with compressibility effects for thick highly cambered multibodies in cascade, noting slotted compressor blade performance

Mikolajczak, A. A.↗

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

Utilization of cascade data in axial-flow compressor design and analysis - A critical review

Axial flow compressor off-design performance optimization by adjustable inlet guide vanes with variable trailing edge flaps

Serovy, G. K.↗

NASA NTRS1970

Intra-stator transport of rotor wakes and its effect on compressor performance

Rotor wakes intrastator transport effects on high Mach number axial flow compressors performance, considering stagnation temperature profile and rotor blade loss factor

Kerrebrock, J. L.↗

NASA NTRS1970