Internal thrust and pumping performance of an auxiliary inlet ejector nozzle with clamshell thrust reverser
Simulated take-off, transonic acceleration, and supersonic flight conditions using auxiliary inlet ejector nozzle
Burley, R. R.↗
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Results for “Inlet”
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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Reingestion characteristics and inlet flow distortion of V/STOL lift-engine fighter configurations.
Exhaust gas reingestion and inlet flow distortion in V/STOL lift engines, discussing static and wind tunnel testing using fighter configuration models
Barrack, J. P.↗
Supersonic wind tunnel investigation of inlet- engine compatibility.
Inlet produced dynamic distortion and effects on stall margin of J-85 turbojet engine from supersonic wind tunnel tests
Calogeras, J. E.↗
A two-dimensional, mixed-compression inlet system designed to self-restart at a Mach number of 3.5.
M 3.5 two dimensional mixed compression inlet system with self restart using flexible variable ramp system
Anderson, W. E.↗
Study of a family of supersonic inlet systems.
Large scale axisymmetric inlet systems performance capabilities, reviewing theoretical and experimental programs
Cubbison, R. W.↗
Inlet effects on boiling and near critical hydrogen heat transfer.
Hydrodynamic inlet conditions effect on film boiling and near critical hydrogen heat transfer, using data from electrically heated various geometry test sections
Brown, D. D.↗
An approximate solution of additive-drag coefficient and mass-flow ratio for inlets utilizing right circular cones at zero angle of attack
Incompressible approximation solution of additive drag coefficient and mass flow ratio for inlets with right circular cones
Mascitti, V. R.↗
Experimental investigation of the effects of pulse pressure distortions imposed on the inlet of a turbofan engine
Pulse pressure distortion effects imposed on inlet of turbofan engine
Wenzel, L. M.↗
Exploratory experimental study of the effects of inlet conditions on the flow and containment characteristics of coaxial flows
Short chamber inlet configuration for eddy elimination in coaxial flow reactor of gaseous core nuclear rockets
Johnson, B. V.↗
An automatic restart control system for an axisymmetric mixed-compression inlet
Automatic restart control system for axisymmetric mixed compression inlet
Cole, G. L.↗
Design and performance of a digital electronic normal shock position sensor for mixed- compression inlets
Digital electronic normal shock position sensor for mixed compression inlets
Cole, G. L.↗
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.↗
Influence of high turbine-inlet temperature and takeoff jet noise on a methane-fueled supersonic transport with variable-sweep wings
Influence of high turbine inlet temperature and take off jet noise on methane fueled supersonic transport with variable swept wings
Kraft, G. A.↗
Effects of inlet-guide-vane configuration and relative blade velocity on noise from axial- flow compressors
Inlet-guide-vane configuration and relative blade velocity effects on noise reduction from axial flow compressors
Chestnutt, D.↗
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.↗
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.↗
Optimization of supersonic inlets using the method of characteristics
Method of characteristics for computerized design of optimal supersonic inlets
Anderson, B. H.↗
Prediction of supersonic and hypersonic inlet flow fields
Computer programs for predicting flow field properties in supersonic and hypersonic inlets
Latham, E. A.↗