Force, Moment, and Flow-field Characteristics of Two Wing-body-nacelle Combinations at Mach Numbers 2 and 3 PDF Download
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Author: Hill, Jr. (William A.)
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 102
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Book Description
Author: Hill, Jr. (William A.)
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 102
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Book Description
Author:
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ISBN:
Category :
Languages : en
Pages : 96
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Author: United States. Superintendent of Documents
Publisher:
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Category : Government publications
Languages : en
Pages : 1714
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Book Description
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index.
Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 1572
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Author: Lyndell S. King
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ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 132
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Wind tunnel tests were conducted to determine the flow distribution about fuselage configurations at transonic and supersonic speeds and at angles of attack up to 20 degrees. The models tested were approximately one-twelfth scale and consisted of a main fuselage forebody member and several attachable components. The components were mounted in several combinations to represent different possible configurations for tactical aircraft. Flow distribution surveys were conducted at two inlet locations ahead of and under the wing to assess the effects of forebody geometry for the conditions indicated. The data indicate the influence of the canopy, nose droop, and fuselage shape on flow angularities in the forward survey plane.
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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Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 818
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Author:
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ISBN:
Category :
Languages : en
Pages : 688
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Author: Dale E. Knutsen
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 72
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Author: Harry W. Carlson
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 78
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