Preliminary Investigation Of Shield To Improve Angle Of Attack Performance Of Nacelle Type Inlet
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Author | : Milton A. Beheim |
Publisher | : |
Total Pages | : 38 |
Release | : 1957 |
Genre | : Airplanes |
ISBN | : |
An investigation was conducted at Mach numbers between 1.6 and 2.0 on the use of a shield along the upper-half periphery of the cowl of a conical inlet to improve performance at angle of attack. The best results were obtained with the shield mounted in such a manner that an air gap existed between the shield and the cowl lip. Zero-angle-of-attack performance was not appreciably affected. At an angle of attack of 8 degrees distortion was about half that without the shield, and subcritical stability was improved.
Author | : |
Publisher | : |
Total Pages | : 494 |
Release | : 1959 |
Genre | : Aeronautics |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 296 |
Release | : 1959 |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 500 |
Release | : 1959 |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 300 |
Release | : 1960 |
Genre | : |
ISBN | : |
Author | : United States. Superintendent of Documents |
Publisher | : |
Total Pages | : 1812 |
Release | : 1960 |
Genre | : Government publications |
ISBN | : |
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 860 |
Release | : 1957 |
Genre | : Aeronautics |
ISBN | : |
Author | : J. Seddon |
Publisher | : AIAA (American Institute of Aeronautics & Astronautics) |
Total Pages | : 440 |
Release | : 1999 |
Genre | : Science |
ISBN | : |
"Intake Aerodynamics, Second Edition" presents computational advancements and discoveries in intake aerodynamics. A companion volume to "Practical Intake Aerodynamic Design," this important text considers the problem of airflow, both internal and external to air intake, as applied to civil and military aircraft. It covers the aerodynamics of subsonic and supersonic intakes in real flows, maintaining a progression through the transonic range. Also considered is the joint perspective of the airframe designer and the propulsion specialist in practical cases. Readers will gain insight into the fluid mechanics behind the deceleration of air from free stream to engine velocity, and an understanding of air compression and external drag in extensively revised chapters reflecting progress in the field. More than 300 drawings and diagrams help to illustrate the points defined throughout the book. Copublished with Blackwell Science Ltd. Outside the United States and Canada, order from Blackwell Science Ltd., United Kingdom, tel 44 1865 206 206.
Author | : E. L. Goldsmith |
Publisher | : AIAA (American Institute of Aeronautics & Astronautics) |
Total Pages | : 472 |
Release | : 1993 |
Genre | : Technology & Engineering |
ISBN | : |
This book provides, for the first time, the distilled experience of authors who have been closely involved in design of air intakes for both airframe and engine manufacturers. Much valuable data from systematic experimental measurements on intakes for missiles, combat, and V/STOL aircraft from research sources in the United Kingdom, the United States, France, and Germany are included, together with the latest developments in computational fluid dynamics applied to air intakes.
Author | : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development |
Publisher | : |
Total Pages | : 272 |
Release | : 1991 |
Genre | : Aerodynamics |
ISBN | : |