Sound measurements on a 4000-pound-thrust high-bypass-ratio turbofan engine
Sound measurements on 4000 pound thrust high bypass ratio turbofan engine
Acker, L. W.↗
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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.↗
Acoustic and aerodynamic performance of a 6-foot-diameter fan for turbofan engines. 1 - Design of facility and QF-1 fan
Design of test facility and prototype fan for turbofan acoustic research
Leonard, B. R.↗
A 90 degree sector development of a short length combustor for a supersonic cruise turbofan engine Interim report, Jun. 1968 - Mar. 1970
Short length combustor and diffuser configuration for supersonic cruise turbofan engine
Clements, T. R.↗
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.↗
Longitudinal aerodynamic characteristics of a twin-turbofan subsonic transport with nacelles mounted under the wings
Longitudinal aerodynamic characteristics of twin-turbofan supersonic transport with nacelles mounted under wings
Capone, F. J.↗
Acoustic and aerodynamic performance of a 6-foot-diameter fan for turbofan engines. 2 - Performance of QF-1 fan in nacelle without acoustic suppression
Low noise turbofan engine without aerodynamic blade loading
Balombin, J. R.↗
Performance of noise suppressors for a full- scale fan for turbofan engines
Performance of noise suppressors for turbofan engines
Rice, E. J.↗
Study and development of turbofan nacelle modifications to minimize fan-compressor noise radiation. Volume 1 - Program summary, 1 May 1967 - 1 November 1969
Turbofan nacelle modifications to minimize fan-compressor noise radiation of Boeing 707 aircraft - Vol. 1
Source record↗
Study and development of turbofan nacelle modifications to minimize fan-compressor noise radiation. Volume 3 - Concept studies and ground tests Contractor report, 1 May 1967 - 1 Nov. 1969
Noise reduction of Boeing 707 during landing approach by modifying turbofan nacelle with polyimide fiber glass acoustic sandwich materials
Source record↗
Study and development of turbofan nacelle modifications to minimize fan-compressor noise radiation. Volume 6 - Economic studies Contractor report, 1 May 1967 - 1 Nov. 1969
Cost analysis of turbofan nacelle modifications to minimize fan-compressor noise radiation
Source record↗
Acoustic and aerodynamic performance of a 6-foot-diameter fan for turbofan engines. 3 - Performance with noise suppressors
Acoustic and aerodynamic performance of six foot diameter fan for turbofan engines with noise suppressors
Acker, L. W.↗
Study and development of turbofan nacelle modifications to minimize fan-compressor noise radiation. Volume 2 - Acoustic lining development, 1 May 1967 - 1 November 1969
Development of acoustic lining for turbofan nacelle modification to minimize fan compressor noise radiation
Source record↗
Experimental performance and combustion stability of a full scale duct burner for a supersonic turbofan engine
Annular diffuser and combustor assembly in full scale duct burner for supersonic turbofan engine
Branstetter, J. R.↗
An investigation of two variations of the gas generator method to calculate the thrust of the afterburning turbofan engines installed in an F-111A airplane
Two variations of gas generator method to calculate thrust of afterburning turbofan engines installed in F-111A aircraft
Burcham, F. W., Jr.↗
Noise measurements for a three engine turbofan transport airplane during climbout and landing approach operations
Climbout and landing approach noise measurements for three engine turbofan transport aircraft
Clark, L. R.↗
Performance of noise suppressors for a full- scale fan for turbofan engines
Turbofan engine noise reduction, using acoustic liners in inlet and exhaust ducts
Rice, E. J.↗
Turbofan STOL research at NASA
Turbofan STOL transport application to air transportation congestion, discussing conditioning landing field length, navigational/control problems and jet flap concepts
Kuhn, R. E.↗