Correlation of flight data on limit pressure coefficients and their relation to high-speed burbling and critical tail loads
Richard V. Rhode
Abstract
Open-access reader
Richard V. Rhode
Abstract
Open-access reader
SPEED nt"'I{B"SII-S-' \I\fD C~n~IC ' ' ,.TJ TA IL LO.•lDS B:r Ri c ha rd v .Rhode F l i~ht d'3.ta are p r 8s p rl t ':3d to .shOWtho t t~e 8.bsolllte minimum ')1' 1 1:11 t rreSSUY'•3 c cef:P2.. c ie!1t on an Ci ir.£>oi1 :. S a func t ion :11n::.n17 of the ':8C1'1 ~-11u:.beJ.• tor ;1<..:.c1' 1 numbar3 above a.bo•u t 0 .3 'nd l:'or 1.~dua l ,2.i,;hc v:lu9s of U:.eHe Vllo 1 d s nl1.rr:ber .rl':1,,: c urve 0:' ].ltrl',~ ::Jr8s:::,ure coeff:'c i ent as c. fU"1ction of ~:l_tch nU.!:1:"er i.G E.stL,hlis:lec. .Tl e f l i~ll t cl•l.t a alDG 1n.l~.c2..te the rat'::) ;,t wl1'eh the ?respure c oeffi c ient decreases wit1'l ctr~Cll:l l.>lcr n'.rn')er as t:-:.e l imi t pr8 ssur3 i oS 3. 'C'urcacLpd "tild wlJ.vn t'J."\ 10c8.1 :. s.ch n umbe r is greater t1:.an un~ ty .Eec811t t}-~e'l l'etic':,.lr33l1 t s of G&rri c k and ~anJan are mod:fi~d a~d extrapo!~t9d in a c co r d&nc r .:;wtth the fli.:::~.-:.t dac''t at t'"e >.:.~::rler 1('23.1 ITa c':l nU.mbe1's
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SPEED nt"'I{B"SII-S-' \I\fD C~n~IC ' ' ,.TJ TA IL LO.•lDS B:r Ri c ha rd v .Rhode F l i~ht d'3.ta are p r 8s p rl t ':3d to .shOWtho t t~e 8.bsolllte minimum ')1' 1 1:11 t rreSSUY'•3 c cef:P2.. c ie!1t on an Ci ir.£>oi1 :. S a func t ion :11n::.n17 of the ':8C1'1 ~-11u:.beJ.• tor ;1<..:.c1' 1 numbar3 above a.bo•u t 0 .3 'nd l:'or 1.~dua l ,2.i,;hc v:lu9s of U:.eHe Vllo 1 d s nl1.rr:ber .rl':1,,: c urve 0:' ].ltrl',~ ::Jr8s:::,ure coeff:'c i ent as c. fU"1ction of ~:l_tch nU.!:1:"er i.G E.stL,hlis:lec. .Tl e f l i~ll t cl•l.t a alDG 1n.l~.c2..te the rat'::) ;,t wl1'eh the ?respure c oeffi c ient decreases wit1'l ctr~Cll:l l.>lcr n'.rn')er as t:-:.e l imi t pr8 ssur3 i oS 3. 'C'urcacLpd "tild wlJ.vn t'J."\ 10c8.1 :. s.ch n umbe r is greater t1:.an un~ ty .Eec811t t}-~e'l l'etic':,.lr33l1 t s of G&rri c k and ~anJan are mod:fi~d a~d extrapo!~t9d in a c co r d&nc r .:;wtth the fli.:::~.-:.t dac''t at t'"e >.:.~::rler 1('23.1 ITa c':l nU.mbe1's
Key concepts: Mach number, Limit (mathematics), Airfoil, Reynolds number, Mathematics, Pressure coefficient, Function (biology), Drag divergence Mach number