CONTRIBUTION OF WING PLANFORM TO DERIVATIVES OF YAWING MOMENT AND SIDEFORCE DUE TO ROLL RATE AT SUBSONIC SPEEDS (Np)w AND (Yp)w.

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Anon

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Engineering Sciences Data Unit, Data Items | 1981年

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Compendex;

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AERODYNAMICS

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[1] ESTIMATION OF SIDEFORCE, YAWING MOMENT AND ROLLING MOMENT DERIVATIVES DUE TO RATE OF ROLL FOR COMPLETE AIRCRAFT AT SUBSONIC SPEEDS.
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[2] CONTRIBUTION OF FIN TO SIDEFORCE, YAWING MOMENT AND ROLLING MOMENT DERIVATIVES TO RATE OF ROLL, (Yp)F, (Np)F, (Lp)F, IN THE PRESENCE OF BODY, WING AND TAILPLANE.
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[3] ESTIMATION OF SIDEFORCE AND YAWING MOMENT DERIVATIVES DUE TO SIDESLIP FOR COMPLETE AIRCRAFT AT SUBSONIC SPEEDS.
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Engineering Sciences Data Unit, Data Items, 1982,
[4] WING-BODY YAWING MOMENT AND SIDEFORCE DERIVATIVES DUE TO SIDESLIP: Nv AND Yv.
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Engineering Sciences Data Unit, Data Items, 1981,
[5] CONTRIBUTION OF BODY TO YAWING MOMENT AND SIDEFORCE DERIVATIVES DUE TO RATE OF YAW, (Nr)B AND (Yr)B.
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Engineering Sciences Data Unit, Data Items, 1983,
[6] CONTRIBUTION OF FIN TO SIDEFORCE, YAWING MOMENT AND ROLLING MOMENT DERIVATIVES DUE TO RATE OF YAW, (Yr)F, (Nr)F, (Lr)F.
Anon
Engineering Sciences Data Unit, Data Items, 1982,