Air Intakes

66 books
Intake aerodynamicsJ. Seddon
⏱ 6h 47m

Intake aerodynamics

J. Seddon

1999407 pp.
Development and testing of a high stability engine control (HISTEC) systemUnknown Author
⏱ 13m

Development and testing of a high stability engine control (HISTEC) system

Unknown Author

199813 pp.
Airflow and thrust calibration of an F100 engine, S/N P680059, at selected flight conditionsThomas J Biesiadny
⏱ 24m

Airflow and thrust calibration of an F100 engine, S/N P680059, at selected flight conditions

Thomas J Biesiadny

197824 pp.
Transonic performance of a Mach 2.65 auxiliary flow axisymmetric inletDon M. Santman
⏱ 1h 1m

Transonic performance of a Mach 2.65 auxiliary flow axisymmetric inlet

Don M. Santman

197661 pp.
Theoretical study of VTOL tilt-nacelle axisymmetric inlet geometriesJ. Dennis Hawk
⏱ 26m

Theoretical study of VTOL tilt-nacelle axisymmetric inlet geometries

J. Dennis Hawk

197926 pp.
The performance of some axi-symmetric isentropic centrebody intakes designed for mach numbers of 2.48 and 3.27E. L. Goldsmith
⏱ 1h 23m

The performance of some axi-symmetric isentropic centrebody intakes designed for mach numbers of 2.48 and 3.27

E. L. Goldsmith

196983 pp.
On the static performance of two-dimensional intakes with momentum injection in the form of boundary-layer control by blowingNigel Gregory
⏱ 57m

On the static performance of two-dimensional intakes with momentum injection in the form of boundary-layer control by blowing

Nigel Gregory

197157 pp.
Inlets and nozzles for aerospace enginesNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Propulsion and Energetics Panel. Meeting

Inlets and nozzles for aerospace engines

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Propulsion and Energetics Panel. Meeting

1971No page data
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.
Experimentelle Untersuchungen des Betriebsverhaltens eines Triebwerkseinlaufs bei Überschall-Anström-MachzahlenThomas Rüggeberg
⏱ 2h 25m

Experimentelle Untersuchungen des Betriebsverhaltens eines Triebwerkseinlaufs bei Überschall-Anström-Machzahlen

Thomas Rüggeberg

1996145 pp.
Lo Schnorchel italianoGino Galuppini
⏱ 2h 9m

Lo Schnorchel italiano

Gino Galuppini

1986129 pp.
Intake aerodynamicsUnknown Author

Intake aerodynamics

Unknown Author

1988No page data
Gazodinamicheskoe konstruirovanie sverkhzvukovykh vozdukhozabornikovV. A. Shchepanovskiĭ
⏱ 3h 44m

Gazodinamicheskoe konstruirovanie sverkhzvukovykh vozdukhozabornikov

V. A. Shchepanovskiĭ

1993224 pp.
Inlet flowfield investigationUnknown Author

Inlet flowfield investigation

Unknown Author

1984No page data
Effects of inlet distortion on a static pressure probe mounted on the engine hub in an F-15 airplaneDonald L. Hughes

Effects of inlet distortion on a static pressure probe mounted on the engine hub in an F-15 airplane

Donald L. Hughes

1985No page data
Final technical report for aeroelastic analysis of propulsion systemsTheo G. Keith

Final technical report for aeroelastic analysis of propulsion systems

Theo G. Keith

1996No page data
Investigation of DC-8 nacelle modifications to reduce fan-compressor noise in airport communitiesMcDonnell Douglas Corporation.

Investigation of DC-8 nacelle modifications to reduce fan-compressor noise in airport communities

McDonnell Douglas Corporation.

1970No page data
Minimum weight design of a generic axisymmetric inletShari-Beth Nadell

Minimum weight design of a generic axisymmetric inlet

Shari-Beth Nadell

1996No page data
Study and development of turbofan nacelle modifications to minimize fan-compressor noise radiationBoeing Company.

Study and development of turbofan nacelle modifications to minimize fan-compressor noise radiation

Boeing Company.

1971No page data
Noise suppression by an acoustically treated three-ring inlet on a TF-34 engineGene L. Minner
⏱ 36m

Noise suppression by an acoustically treated three-ring inlet on a TF-34 engine

Gene L. Minner

197636 pp.
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