Static Aerodynamic Characteristics of a Short Blunt 10 Degree Semivertex Angle Cone at a Mach Number of 15 in Helium PDF Download
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Author: Melvin J. Fohrman
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 48
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Book Description
Author: Melvin J. Fohrman
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 48
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Book Description
Author: Melvin J. Fohrman
Publisher:
ISBN:
Category :
Languages : en
Pages : 37
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Book Description
Author: Melvin J. Fohrman
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 37
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Book Description
Author: J. Wayne Keyes
Publisher:
ISBN:
Category : Cone
Languages : en
Pages : 72
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Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 542
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Book Description
Author: Stuart L. Treon
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 40
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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 : 260
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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. Department of Commerce. Office of Technical Services
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 836
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Book Description
Author: E. L. Clark
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 98
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Book Description
The pressure distribution predicted by the modified Newtonian theory is used to develop equations for the aerodynamic forces, moments, and stability derivatives for components of hypersonic lifting configurations. In conjunction with the equations, a set of charts is presented to enable simple determination of the aerodynamic characteristics of swept cylinders, swept wedges, spherical segments, and cone frustums at zero sideslip and angles of attack from 0 to 180 degrees. This method allows evaluation of most delta wing-body combinations without the need for numerical or graphical integration. As an example of the procedure, the theoretical characteristics of a blunt 75-degree swept delta wing are calculated and compared with experimental results.
