Lift, drag, and hinge moments at supersonic speeds of an all-movable triangular wing and body combination Page: 4 of 40
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NACA RM A 5322
KB(W)
kB(w)
KW(B)
kW(B)
M
R
Cr
Cr/gT correction to cdc for finite length
Subscriptsbody (exclusive of nose) in presence of wing
experiment
hinge line
minimumlift-ratio parameters for body nose, body in presence of wing,
and wing in presence of body
(See ref. I for complete definitions.)
Mach number
dynamic pressure, lb/sq in.
Reynolds number, based on body length
body cross-section area, sq in.
distance from leading edge of wing-body Juncture to center of
pressure of wing panel in fraction of wing root chord
distance from leading edge of wing-body Juncture to hinge line
in fraction of root chord
distance of center of pressure of the wing panel from the hinge
line in fraction of mean aerodynamic chord
angle of attack, deg
angle of attack for minimum drag, deg
wing deflection angle, deg
relative effectiveness of the wing in tift, exr
(CL)theoTI
4B(W)
exp
H
min3
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Drake, William C. Lift, drag, and hinge moments at supersonic speeds of an all-movable triangular wing and body combination, report, September 16, 1953; (https://digital.library.unt.edu/ark:/67531/metadc59734/m1/4/: accessed March 28, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.