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An investigation of the velocity distribution around the nose of the aerofoil with a ﬂap
aerodynamic aerofoil aileron aircraft amplitude angle approximately aspect ratio blade boundary layer calculated cent chord chordwise coefﬁcient coefficients conﬁguration constant contact surface cooling curve deﬁned delta wings derivatives diameter diaphragm distribution downstream drag effect elevator engine equation experimental ﬁrst ﬂight ﬂutter speed frequency ft/sec given heat holes hull increase inertia inﬂuence integral knots laminar ﬂow leading edge length Mach number mass-balance maximum measured method modiﬁcations Nusselt obtained oscillating parameter perforations pitch pitot pressure Prof proﬁle rarefaction rarefaction wave reﬂected region Reynolds number rotor Sea Venom shaft shock tube shock wave shock-tube shown in Fig singular solution slots spanwise spring-tab static stator step stiffness supersonic sweepback Table tailplane take-off temperature tests theoretical thyratron trailing edge transition trim-tab tunnel two-dimensional upstream values valve variation velocity proﬁles viscosity working-section zero