Experimental Aerodynamic Characteristics for Slender Bodies with Thin Wings and Tail at Angles of Attack from 0 ̊to 58 ̊and Mach from 0.6 to 2.0 PDF Download
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Author: Leland H. Jorgensen
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 236
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Book Description
Author: Leland H. Jorgensen
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 236
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 978
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 732
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Book Description
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1388
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Book Description
Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : United States
Languages : en
Pages : 1408
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Book Description
Author: Robert J. Krieger
Publisher:
ISBN:
Category : Cruise missiles
Languages : en
Pages : 136
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Book Description
This report presents the results of a program that investigated aerodynamic configuring as a method of improving long range supersonic cruise and maneuvering missile performance. Non-circular body, lifting body, blended wing body, wing-body and favorable interference concepts were developed and wind tunnel tested. Substantial improvements in cruise range were shown to result from aero configuring.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1146
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1008
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Book Description
Beginning Oct. 1959 some issues include "Russian supplement."
Author: American Rocket Society
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 1068
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Book Description
Supplements accompany some issues.
Author:
Publisher:
ISBN:
Category : Rocketry
Languages : en
Pages : 512
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Book Description
Beginning Oct. 1959 some issues include "Russian supplement."
