An Analysis of the Delta-wing Hypersonic Stability and Control Behavior at Angles of Attack Between 30° and 90° PDF Download
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Author: David E. Fetterman
Publisher:
ISBN:
Category : Delta wing airplanes
Languages : en
Pages : 72
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Book Description
Author: David E. Fetterman
Publisher:
ISBN:
Category : Delta wing airplanes
Languages : en
Pages : 72
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Book Description
Author: David E. Fetterman
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
Author: David E. Fetterman
Publisher:
ISBN:
Category : Delta wing airplanes
Languages : en
Pages : 58
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Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 58
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Book Description
Author: Norman D. Malmuth
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 54
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Author: Arnold Polak
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 48
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Book Description
The flow of a perfect gas over the slab portion of a blunted delta wing flying at hypersonic speeds is studied. A set of approximate equations is derived and a solution - for an inviscid flow - is obtained. Using this solution as a representation for the inviscid flow problem, a formulation to the laminar boundary-layer equations is presented; one which is applicable to the flow field's azimuthal planes where the crossflow gradients are not too large. Numerical solutions to these boundary-layer equations have been obtained; however, these are restricted to the azimuthal planes and near to the leading edges. The results indicate the presence of a dividing surface streamline since a numerical solution could not be obtained near the centerplane of the wing, where the crossflow velocity is large. (Author).
Author: James Campbell Robinson
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 76
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Author: Gloria Hernandez
Publisher:
ISBN:
Category : Leading edge flaps
Languages : en
Pages : 112
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 936
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Author: John B. McDevitt
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 114
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