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Author: United States. Federal Aviation Agency
Publisher:
ISBN:
Category :
Languages : en
Pages : 39
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Book Description
Some preliminary accomplishments of sonic boom research in predicting strength and location of sonic boom shock waves, determining the effects on light aircraft, and evaluating community tolerance to various levels of sonic boom intensity are reviewed. A brief summary of the implications of sonic boom with regard to supersonic transport design is included.
Author: United States. Federal Aviation Agency
Publisher:
ISBN:
Category :
Languages : en
Pages : 39
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Book Description
Some preliminary accomplishments of sonic boom research in predicting strength and location of sonic boom shock waves, determining the effects on light aircraft, and evaluating community tolerance to various levels of sonic boom intensity are reviewed. A brief summary of the implications of sonic boom with regard to supersonic transport design is included.
Author: Louise K. Annus
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 120
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Book Description
Author: Henning E. von Gierke
Publisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 14
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Book Description
Author: United States. Congress. House. Committee on Foreign Affairs
Publisher:
ISBN:
Category :
Languages : en
Pages : 1158
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Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 94
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Book Description
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 496
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Book Description
Author: John Henry Wiggins
Publisher:
ISBN:
Category : Sonic boom
Languages : en
Pages : 192
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Book Description
Author: Harvey H. Hubbard
Publisher:
ISBN:
Category : Sonic boom
Languages : en
Pages : 52
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Book Description
Author: Harvey H. Hubbard
Publisher:
ISBN:
Category : Sonic boom
Languages : en
Pages : 56
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Book Description
The U.S. Air Force, National Aeronautics and Space Administration, and Federal Aviation Agency have engaged in a joint research program for the purpose of measuring sonic-boom pressure signatures. These measurements are presented for several locations for flight tests of fighter and bomber airplanes in the altitude range from about 10,000 to 75,000 feet and at Mach numbers from 1.1 to 2.0. Data were obtained for a variety of atmospheric wind and temperature gradients and for various flight paths and acceleration rates.
Author: United States. Panel on Noise Abatement
Publisher:
ISBN:
Category : Noise control
Languages : en
Pages : 312
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Book Description
