Investigation of a Twisted Cambered Wing with a 750 Swept Leading Edge at Mach 3 and Reynolds Numbers to 39 X 106 PDF Download
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Author: John A. Moore
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 34
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Book Description
Author: John A. Moore
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 34
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Book Description
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1128
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Book Description
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1440
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Book Description
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 258
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Book Description
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 448
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Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 980
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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 : 1426
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 650
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Book Description
