Air Intakes

66 books
Ingestion of debris into intakes by vortex actionD. E. Glenny
⏱ 27m

Ingestion of debris into intakes by vortex action

D. E. Glenny

197027 pp.
Preliminary investigation of a new type of supersonic inletFerri, Antonio
⏱ 19m

Preliminary investigation of a new type of supersonic inlet

Ferri, Antonio

195319 pp.
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
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
Tests with a two-dimensional intake having all-external compression and a design mach number of 2.2 [sic, i.e. 2.0]M. C. Neale
⏱ 17m

Tests with a two-dimensional intake having all-external compression and a design mach number of 2.2 [sic, i.e. 2.0]

M. C. Neale

196717 pp.
Boundary-layer interaction effects in intakes with particular reference to those designed for dual subsonic and supersonic performanceJ. Seddon
⏱ 22m

Boundary-layer interaction effects in intakes with particular reference to those designed for dual subsonic and supersonic performance

J. Seddon

197022 pp.
Supersonic inletsIone D. V. Faro
⏱ 2h 38m

Supersonic inlets

Ione D. V. Faro

1965158 pp.
Analysis of ejectors used as supersonic propelling nozzles for jet enginesBengt Ahrén
⏱ 3h 15m

Analysis of ejectors used as supersonic propelling nozzles for jet engines

Bengt Ahrén

1968195 pp.
Measurement of the internal drag of air breathing installations on slender wing-body combinations at supersonic speedsJ. W. Britton
⏱ 17m

Measurement of the internal drag of air breathing installations on slender wing-body combinations at supersonic speeds

J. W. Britton

196717 pp.
Theoretical and experimental analysis of low-drag supersonic inlets having a circular cross section and a central body at Mach numbers of 3.30, 2.75, and 2.45Ferri, Antonio
⏱ 37m

Theoretical and experimental analysis of low-drag supersonic inlets having a circular cross section and a central body at Mach numbers of 3.30, 2.75, and 2.45

Ferri, Antonio

195537 pp.
Internal performance of a variable ramp mixed compression intake at Mach 3.05S. A. Fisher
⏱ 10m

Internal performance of a variable ramp mixed compression intake at Mach 3.05

S. A. Fisher

198510 pp.
Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controled inlet-stability bypass system when subjected to internal and external airflow transientsBobby W Sanders
⏱ 1h 38m

Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controled inlet-stability bypass system when subjected to internal and external airflow transients

Bobby W Sanders

198098 pp.
Experimental evaluation of a spinning-mode acoustic-treatment design concept for aircraft inletsLaurence J Heidelberg
⏱ 26m

Experimental evaluation of a spinning-mode acoustic-treatment design concept for aircraft inlets

Laurence J Heidelberg

198026 pp.
Simulated flight effects on noise characteristics of a fan inlet with high throat Mach numberHoward L. Wesoky
⏱ 42m

Simulated flight effects on noise characteristics of a fan inlet with high throat Mach number

Howard L. Wesoky

197842 pp.
Tests on an engine installation for a slender gothic wing at M-1.82R. T. Griffiths
⏱ 21m

Tests on an engine installation for a slender gothic wing at M-1.82

R. T. Griffiths

196721 pp.
Airframe/propulsion interferenceNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel. Symposium

Airframe/propulsion interference

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel. Symposium

1975No page data
Simulated flight effects on noise characteristics of a fan inlet with high throat Mach numberHoward L Wesoky
⏱ 42m

Simulated flight effects on noise characteristics of a fan inlet with high throat Mach number

Howard L Wesoky

197842 pp.
Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inletsCharles J. Trefny
⏱ 1h 0m

Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets

Charles J. Trefny

198660 pp.
Theoretical flow characteristics of inlets for tilting-nacelle VTOL aircraftMichael A. Boles
⏱ 29m

Theoretical flow characteristics of inlets for tilting-nacelle VTOL aircraft

Michael A. Boles

197829 pp.
Investigation of a mixed-compression axisymmetric inlet system at Mach numbers 0.6 to 3.5Donald B. Smeltzer
⏱ 4h 2m

Investigation of a mixed-compression axisymmetric inlet system at Mach numbers 0.6 to 3.5

Donald B. Smeltzer

1970242 pp.
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