Air Intakes

66 books
Practical intake aerodynamic designE. L. Goldsmith
⏱ 7h 14m

Practical intake aerodynamic design

E. L. Goldsmith

1993434 pp.
Turbojet-exhaust-nozzle secondary-airflow pumping as an exit control of an inlet-stability bypass system for a Mach 2.5 axisymmetric mixed-compression inletBobby W. Sanders
⏱ 1h 18m

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

Bobby W. Sanders

198078 pp.
Inlet flow characteristics during rapid maneuvers for an F/A-18A airplaneWilliam G. Steenken

Inlet flow characteristics during rapid maneuvers for an F/A-18A airplane

William G. Steenken

1999No page data
Low-speed aerodynamic test of an axisymmetric supersonic inlet with variable cowl slotA. G. Powell

Low-speed aerodynamic test of an axisymmetric supersonic inlet with variable cowl slot

A. G. Powell

1985No page data
An experimental investigation of the flow through inclined circular tubes at a mach number of 4.0P. L. Roe
⏱ 16m

An experimental investigation of the flow through inclined circular tubes at a mach number of 4.0

P. L. Roe

196616 pp.
Air intake problems in supersonic propulsionNorth Atlantic Treaty Organization. Combustion and Propulsion Panel.
⏱ 1h 22m

Air intake problems in supersonic propulsion

North Atlantic Treaty Organization. Combustion and Propulsion Panel.

195882 pp.
Intake aerodynamicsJ. Seddon
⏱ 6h 47m

Intake aerodynamics

J. Seddon

1999407 pp.
More tests with a variable ramp intake having a design mach number of 2.2M. C. Neale
⏱ 16m

More tests with a variable ramp intake having a design mach number of 2.2

M. C. Neale

196716 pp.
Some tests with a variable ramp intake having sidewall compression and a design mach number of 2.2M. C. Neale

Some tests with a variable ramp intake having sidewall compression and a design mach number of 2.2

M. C. Neale

1967No page data
Three-dimensional compressible turbulent computations for a nondiffusing S-ductUnknown Author

Three-dimensional compressible turbulent computations for a nondiffusing S-duct

Unknown Author

1992No page data
Aerodynamic and directional acoustic performance of a scoop inletJohn M Abbott
⏱ 26m

Aerodynamic and directional acoustic performance of a scoop inlet

John M Abbott

197826 pp.
Turbojet-exhaust-nozzle secondary-airflow pumping as an exit control of an inlet-stability bypass system for a Mach 2.5 axisymmetric mixed-compression inletBobby W Sanders
⏱ 1h 18m

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

Bobby W Sanders

198078 pp.
Inlet spillage drag tests and numerical flow-field analysis at subsonic and transonic speeds of a 1/8-scale, two-dimensional, external-compression, variable-geometry supersonic inlet configurationJoseph E. Hawkins
⏱ 1h 46m

Inlet spillage drag tests and numerical flow-field analysis at subsonic and transonic speeds of a 1/8-scale, two-dimensional, external-compression, variable-geometry supersonic inlet configuration

Joseph E. Hawkins

1976106 pp.
Turbojet-exhaust-nozzle secondary-airflow pumping as an exit control of an inlet-stability bypass system for a Mach 2.5 axisymmetric mixed-compression inletBobby W Sanders
⏱ 1h 18m

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

Bobby W Sanders

198078 pp.
Practical intake aerodynamic designE. L. Goldsmith
⏱ 7h 14m

Practical intake aerodynamic design

E. L. Goldsmith

1993434 pp.
Inlets for supersonic missilesJohn J. Mahoney
⏱ 3h 57m

Inlets for supersonic missiles

John J. Mahoney

1990237 pp.
Noise suppression with high Mach number inletsEdward Lumsdaine
⏱ 1h 40m

Noise suppression with high Mach number inlets

Edward Lumsdaine

1976100 pp.
Effect of simulated downstream flow blockage doors on the performance of an axial-flow fan rotorWalter Martin Osborn
⏱ 25m

Effect of simulated downstream flow blockage doors on the performance of an axial-flow fan rotor

Walter Martin Osborn

197025 pp.
Wind-tunnel tests on a rectangular, twin-duct, variable-geometry air intakeM. D. Dobson
⏱ 52m

Wind-tunnel tests on a rectangular, twin-duct, variable-geometry air intake

M. D. Dobson

196752 pp.
Ingestion of debris into intakes by vortex actionD. E. Glenny
⏱ 27m

Ingestion of debris into intakes by vortex action

D. E. Glenny

197027 pp.
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