WING-BODY YAWING MOMENT AND SIDEFORCE DERIVATIVES DUE TO SIDESLIP: Nv AND Yv.

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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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摘要：

AERODYNAMICS

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[1] 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,
[2] EFFECTS OF ISOLATED BODY AND WING-BODY INTERFERENCE ON ROLLING MOMENT DUE TO SIDESLIP.
Anon
Engineering Sciences Data Unit, Data Items, 1981,
[3] CONTRIBUTION OF BODY TO YAWING MOMENT AND SIDEFORCE DERIVATIVES DUE TO RATE OF YAW, (Nr)B AND (Yr)B.
Anon
Engineering Sciences Data Unit, Data Items, 1983,
[4] CONTRIBUTION OF WING PLANFORM TO DERIVATIVES OF YAWING MOMENT AND SIDEFORCE DUE TO ROLL RATE AT SUBSONIC SPEEDS (Np)w AND (Yp)w.
Anon
Engineering Sciences Data Unit, Data Items, 1981,
[5] ESTIMATION OF SIDEFORCE, YAWING MOMENT AND ROLLING MOMENT DERIVATIVES DUE TO RATE OF ROLL FOR COMPLETE AIRCRAFT AT SUBSONIC SPEEDS.
Anon
Engineering Sciences Data Unit, Data Items, 1985,
[6] AERO-NORMALISED STABILITY DERIVATIVES: EFFECT OF WING ON YAWING MOMENT DUE TO YAWING.
Anon
Engineering Sciences Data Unit, Data Items, 1971,
[7] 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.
Anon
Engineering Sciences Data Unit, Data Items, 1983,
[8] THE ROLLING MOMENT DUE TO SIDESLIP FOR A SWEPT WING
MILES, JW
JOURNAL OF THE AERONAUTICAL SCIENCES, 1948, 15 (07): : 418 - 424
[9] 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,
[10] LIFT AND ROLLING MOMENT ON A SLENDER WING-BODY COMBINATION WITH A DEFLECTED TIP CONTROL
CLARKE, JF
JOURNAL OF THE AERONAUTICAL SCIENCES, 1958, 25 (03): : 203 - 205