1-24 of 56 Books
Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets
Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets
By Charles J. Trefny
Turbojet-exhaust-nozzle secondary-airflow pumping as an exit control of an inlet-stability bypass system for a Mach 2.5 axisymmetric mixed-compression inlet
Turbojet-exhaust-nozzle secondary-airflow pumping as an exit control of an inlet-stability bypass system for a Mach 2.5 axisymmetric mixed-compression inlet
By Bobby W. Sanders
Low-speed aerodynamic test of an axisymmetric supersonic inlet with variable cowl slot
Low-speed aerodynamic test of an axisymmetric supersonic inlet with variable cowl slot
By A. G. Powell
Tests with a two-dimensional intake having all-external compression and a design mach number of 2.2 [sic, i.e. 2.0]
Tests with a two-dimensional intake having all-external compression and a design mach number of 2.2 [sic, i.e. 2.0]
By M. C. Neale
Simulated flight effects on noise characteristics of a fan inlet with high throat Mach number
Simulated flight effects on noise characteristics of a fan inlet with high throat Mach number
By Howard L. Wesoky
Numerical simulation of helicopter engine plume in forward flight
Numerical simulation of helicopter engine plume in forward flight
By Arsenio C. B. Dimanlig
Inlet flow characteristics during rapid maneuvers for an F/A-18A airplane
Inlet flow characteristics during rapid maneuvers for an F/A-18A airplane
By William G. Steenken
Theoretical flow characteristics of inlets for tilting-nacelle VTOL aircraft
Theoretical flow characteristics of inlets for tilting-nacelle VTOL aircraft
By Michael A. Boles
Mach 10 experimental database of a three-dimensional scramjet inlet flow field
Mach 10 experimental database of a three-dimensional scramjet inlet flow field
By Scott D. Holland
Noise suppression with high Mach number inlets
Noise suppression with high Mach number inlets
By Edward Lumsdaine
Boundary-layer interaction effects in intakes with particular reference to those designed for dual subsonic and supersonic performance
Boundary-layer interaction effects in intakes with particular reference to those designed for dual subsonic and supersonic performance
By J. Seddon
The performance of some axi-symmetric isentropic centrebody intakes designed for mach numbers of 2.48 and 3.27
The performance of some axi-symmetric isentropic centrebody intakes designed for mach numbers of 2.48 and 3.27
By E. L. Goldsmith
Effect of simulated downstream flow blockage doors on the performance of an axial-flow fan rotor
Effect of simulated downstream flow blockage doors on the performance of an axial-flow fan rotor
By Walter Martin Osborn
Investigation of DC-8 nacelle modifications to reduce fan-compressor noise in airport communities
Investigation of DC-8 nacelle modifications to reduce fan-compressor noise in airport communities
By McDonnell Douglas Corporation.
Study and development of turbofan nacelle modifications to minimize fan-compressor noise radiation
Study and development of turbofan nacelle modifications to minimize fan-compressor noise radiation
By Boeing Company.
Tests on an engine installation for a slender gothic wing at M-1.82
Tests on an engine installation for a slender gothic wing at M-1.82
By R. T. Griffiths
On the static performance of two-dimensional intakes with momentum injection in the form of boundary-layer control by blowing
On the static performance of two-dimensional intakes with momentum injection in the form of boundary-layer control by blowing
By Nigel Gregory
An experimental investigation of the flow through inclined circular tubes at a mach number of 4.0
An experimental investigation of the flow through inclined circular tubes at a mach number of 4.0
By P. L. Roe
More tests with a variable ramp intake having a design mach number of 2.2
More tests with a variable ramp intake having a design mach number of 2.2
By M. C. Neale
Some tests with a variable ramp intake having sidewall compression and a design mach number of 2.2
Some tests with a variable ramp intake having sidewall compression and a design mach number of 2.2
By M. C. Neale
Investigation of a mixed-compression axisymmetric inlet system at Mach numbers 0.6 to 3.5
Investigation of a mixed-compression axisymmetric inlet system at Mach numbers 0.6 to 3.5
By Donald B. Smeltzer
Analysis of ejectors used as supersonic propelling nozzles for jet engines
Analysis of ejectors used as supersonic propelling nozzles for jet engines
By Bengt Ahrén
Wind-tunnel tests on a rectangular, twin-duct, variable-geometry air intake
Wind-tunnel tests on a rectangular, twin-duct, variable-geometry air intake
By M. D. Dobson