Author: Edward C. Polhamus
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 90
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Book Description
A summary and analysis has been made of results obtained in a systematic research program concerned with the effects of wing sweep, aspect ratio, taper ratio, and dihedral on the rolling moment due to sideslip characteristics of wing-fuselage configurations up to Mach numbers of about 0.95. Other test results are presented to show trends of rolling moment due to sideslip with Mach number for a few wings in the transonic and supersonic speed range.
Author: Edward Charles Polhamus
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 86
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Book Description
Author: Edward C. Polhamus
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 81
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 696
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 750
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Author: Lewis R. Fisher
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44
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Book Description
A method which has previously been presented for the estimation of the low-speed stability derivatives of swept wings is modified to yield approximate corrections for the first-order three-dimensional effects of compressible flow in the subsonic region. Corrections are presented in chart for for several aspect ratios and angles of sweep. Lift-curve slopes and values of damping roll are compared with those obtained by use of a generally accepted method and are discussed in relation to unpublished data.
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category :
Languages : en
Pages : 498
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 494
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Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category :
Languages : en
Pages : 300
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