Evaluation with a turbofan engine of air jets as a steady-state inlet flow distortion device Technical memorandum
Turbofan engine used for evaluating air jets as steady state inlet flow distortion device
Braithwaite, W. M.↗
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Performance of short length turbojet combustor insensitive to radial distortion of inlet airflow
Performance of short length turbojet combustor insensitive to radial distortion of inlet airflow
Humenik, F. M.↗
Performance and stall limits of an afterburner-equipped turbofan engine with and without inlet flow distortion
Performance and stall limits of afterburner-type turbofan engine with and without inlet flow distortion
Abdelwahab, M.↗
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.↗
Reduction of alternator apparent-power requirements and harmonic distortion caused by phase-controlled parasitic loads
Reduction of alternator apparent power requirements and harmonic distortion caused by phase-controlled parasitic loads
Gilbert, L. J.↗
Device for producing dynamic distortion patterns at inlets of air-breathing engines
Producing dynamic distortion patterns at inlets of air-breathing engines
Baumbrick, R. J.↗
Evaluation of range and distortion tolerance for high Mach number transonic stages
Designing transonic compressors for investigating distortion tolerance of high tip speed fan stages
Doyle, V. L.↗
The rate distortion function for a class of sources
Rate distortion function for class of sources, proving positive and negative sides of Shannon encoding theorem for noisy channels
Sakrison, D. J.↗
Distortion of a narrow-band FM signal in a lossless abrupt-junction nonoverdriven varactor doubler
Narrow bandwidth FM signal distortion during multiplication in lossless varactor multiplier calculated, using equivalent circuit of frequency doubler
Grayzel, A. I.↗
Rate distortion function for a Gaussian source model of images
Gaussian source model of image, deriving rate distortion function under mean square error criterion
Habibi, A.↗
Pattern distortion due to edge diffractions
Microwave aperture antenna in finite size ground plane, calculating radiation pattern distortion by superposition of boundary value and wedge diffraction solutions
Balanis, C. A.↗
Dynamic distortion at the exit of a subsonic diffuser of a mixed compression inlet
Measuring distortion characteristics at engine face station of axisymmetric inlet
Kostin, L. C.↗
Reingestion characteristics and inlet flow distortion of V/STOL lift-engine fighter configurations
Reingestion characteristics and inlet flow distortion of V/STOL fighter powered by J-85 engine
Barrack, J. P.↗
Undistorted inlet flow testing. Evaluation of range and distortion tolerance for high Mach number transonic fan stages, volume 1 Task 2 stage data and performance report
Evaluation of range and distortion tolerance for high Mach number transonic fan stages - Vol. 1
Bilwakesh, K. R.↗
Undistorted inlet flow testing. Evaluation of range and distortion tolerance for high Mach number transonic fan stages, volume 2 Task 2 stage data and performance report
Evaluation of range and distortion tolerance for high Mach number transonic fan stages - Vol. 2
Bilwakesh, K. R.↗
Effect of various diffuser designs on the performance of an experimental turbojet combustor insensitive to radial distortion of inlet airflow
Effect of various diffuser designs on performance of experimental turbojet combustor insensitive to radial distortion of inlet airflow
Biaglow, J. A.↗
Experimental investigation of the effect of screen induced total pressure distortion on turbojet stall margin
Effect of circumferential, radial, and combined pressure distortions on stall margin of J-85 engine
Burstadt, P. L.↗
Thermal active optics technique for correcting symmetrical distortions in space telescope mirrors
Thermal active optics technique for correcting symmetrical distortions in space telescope mirrors with analytical demonstration on beryllium paraboloid
Rhodes, M. D.↗