Potential flow solutions for inlets of VTOL lift fans and engines
Potential flow solution for VTOL inlets in static and crossflow operation
Stockman, N. O.↗
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Single stage experimental evaluation of variable geometry inlet guide vanes and stator blading, part 6 Final report
Variable geometry inlet guide vanes and stators for extending stable operation of supersonic cruise turbine engine compressor front stage
Jones, B. A.↗
Preliminary performance of a Brayton-cycle- power-system gas loop operating with krypton over a turbine inlet temperature range of 1200 F to 1600 F
Brayton cycle power system gas loop operating with krypton over turbine inlet temperature of 1200 F to 1600 F
Asadourian, A. S.↗
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.↗
Static performance of an auxiliary inlet ejector nozzle using an afterburning turbojet gas generator
Performance characteristics of auxiliary inlet ejector nozzle configurations for takeoff, transonic acceleration, and supersonic flight conditions with pressure and temperature profiles
Burley, R. R.↗
Flight performance of auxiliary inlet ejector and plug nozzle at transonic speeds
Flight performance of auxiliary inlet ejector and plug nozzle at transonic speeds
Burley, R. R.↗
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.↗
Increasing the stable operating range of a Mach 2.5 inlet
Wind tunnel tests to increase stable operating range of supersonic mixed compression inlet
Mitchell, G. A.↗
Experimental investigation of a large scale, two-dimensional, mixed-compression inlet system - Performance at design conditions, M=3.0
Wind tunnel experiments on large scale, two dimensional, mixed compression inlet systems operating at Mach 3
Anderson, W. E.↗
Performance of an aerodynamically positioned auxiliary inlet ejector nozzle at Mach numbers from 0 to 2.0
Performance of aerodynamically positioned auxiliary inlet ejector nozzle at Mach numbers from 0 to 2.0
Bresnahan, D. L.↗
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.↗
Investigation of a digital simulation of the XB-70 inlet and its application to flight- experienced free-stream disturbances at Mach numbers of 2.4 to 2.6
Digital simulation program to predict atmospheric turbulence effects on inlet system of XB-70 aircraft
Gallagher, R. J.↗
Performance of an auxiliary inlet ejector nozzle with fixed doors and single-hinge trailing-edge flap
Auxiliary inlet ejector nozzle with fixed doors and single-hinge trailing-edge flaps
Johns, A. L.↗
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.↗
XB-70 flight test data comparisons with simulation predictions of inlet unstart and buzz
XB-70 flight test data comparison with simulated predictions of inlet unstart and buzz
Beaulieu, W. D.↗
Performance of a fixed geometry wind tunnel model of an auxiliary inlet ejector with a clamshell flow diverter from Mach 0 to 1.2
Fixed geometry wind tunnel model of auxiliary inlet ejector with clamshell flow diverter from Mach 0 to 1.2
Johns, A. L.↗
Inlet deflector for jet engines Patent
Deflector for preventing objects from entering nacelle inlets of jet aircraft
Olson, W. T.↗
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.↗