Comparison between prediction and experiment for all-movable wing and body combinations at supersonic speeds: Lift, pitching moment, and hinge moment Page: 4 of 43
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NACA RM A52D29(- 3
Chs rate of change of hinge-moment coefficient with wing deflection
(0 , per radian
CL lift coefficient L
CL lift-curve slope for angle of attack( , per radian
CLlift-curve slope for wing deflection angle , per radan
radian
<CL w lift-curve slope due to angle of attack of wing alone, perradian
qg pitching-moment coefficient about body nose -
OmC pitching-moment--curve slope for angle of attack peCmr
radian ' per
r Cm8 pitching-moment-curve slope for wing deflection angle ,
per radian
cr chord at wing-fuselage juncture, inches
ct chord at wing tip, inches
d body diameter, inches
g gap between wing and body, inches
H hinge moment, pound-inches
kB) L() for zero angle of attack and varying wing deflection
angle
k'B(W) approximate value of kB(W)
kW(B LW(B) for zero angle of attack and varying wing deflection
angle
KB(W) Lg (w) for zero wing deflection angle and varying angle of
attack
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Nielsen, Jack N.; Kaattari, George E. & Drake, William C. Comparison between prediction and experiment for all-movable wing and body combinations at supersonic speeds: Lift, pitching moment, and hinge moment, report, August 8, 1952; (https://digital.library.unt.edu/ark:/67531/metadc64451/m1/4/: accessed April 25, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.