Current Papers, Issues 1040-1064H.M. Stationery Office, 1969 - Aeronautics |
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Common terms and phrases
adverse pressure gradients aerodynamic aeroelastic AERONAUTICAL RESEARCH COUNCIL afterbody aircraft airspeed analysis angle Appendix approximate autostabiliser axis calculated calibration chord coefficient components constant cross-flow curves density DETACHABLE ABSTRACT CARDS distributed load drag duct edge effect engines estimated Event in flight factor fluid frequency given H₂ heat transfer inches incidence increment input integral equations jet tube laminar lift lift coefficient longitudinal lower surface M₁ Mach number MAJESTY'S STATIONERY OFFICE maximum measurements method MINISTRY OF TECHNOLOGY momentum integral equations N₂ nacelle nonlinear normal acceleration nozzle Nusselt obtained oscillation oscillatory parameter pitching moment plate pressure gradients problems profiles R.A.E. Technical rate of pitch ratio reference Reynolds number rotating Royal Aircraft Establishment secondary flow shear shock shown skin friction solution speed strain gauge streamwise Street stress supersonic swept wing tailplane take-off tension turbulent variation velocity wall wall-jet wind tunnel zero