Supersonic Lateral-directional Stability Characteristics of a 45 ̊swept Wing-body-tail Model with Various Body Cross-sectional Shapes PDF Download

Author: Dennis E. Fuller
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 54

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Author: United States. National Aeronautics and Space Administration
Publisher:
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Category :
Languages : en
Pages :

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Author:
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ISBN:
Category :
Languages : en
Pages : 78

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Author: Dennis E. Fuller
Publisher:
ISBN:
Category :
Languages : en
Pages : 43

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Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 1068

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Author: James F. Campbell
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Category :
Languages : en
Pages : 71

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Author: M. Leroy Spearman
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 34

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An investigation has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determine the effects of wing and horizontal-tail vertical location on the aerodynamic characteristics in sideslip at various angles of attack for a supersonic airplane configuration at Mach numbers of 1.41 and 2.01. The basic model was equipped with a wing and horizontal tail, each having 45 degree sweep and an aspect ratio of 4. The wing had a taper ratio of 0.2 and NACA 65A004 sections; the horizontal tail had a taper ratio of 0.4 and NACA 65A006 sections.

Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1592

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Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1152

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Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 666

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