transonic aerodynamic

  • 61Jet engine — For a general overview of aircraft engines, see Aircraft engine. A Pratt Whitney F100 turbofan engine for the …

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  • 62List of military aircraft of the United States — This list of military aircraft of the United States includes prototype, pre production and operational types. For aircraft in service, see the List of active United States military aircraft. Prototypes are normally prefixed with X and are often… …

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  • 63Compressibility — This article is about thermodynamics and fluid mechanics. For other uses, see Compression (disambiguation). Incompressibility redirects here. For the property of vector fields, see Solenoidal vector field. Thermodynamics …

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  • 64English Electric Lightning — Infobox Aircraft name= Lightning caption= A Lightning F.3 in 1964 type= Interceptor manufacturer= English Electric British Aircraft Corporation designer= Teddy Petter first flight= 4 August avyear|1954 (P.1A) 4 April avyear|1957 introduced=… …

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  • 65Vortex generator — A vortex generator is an aerodynamic surface, consisting of a small vane that creates a vortex.Peppler, I.L.: From The Ground Up , page 23. Aviation Publishers Co. Limited, Ottawa Ontario, Twenty Seventh Revised Edition, 1996. ISBN 09690054 9 0]… …

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  • 66Fourth generation jet fighter — Lockheed Martin F 16. Dassault Mirage …

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  • 67Airspeed indicator — The airspeed indicator or airspeed gauge is an instrument used in an aircraft to display the craft s airspeed, typically in knots, to the pilot. Markings Light aircraft Airspeed indicator markings use a set of standardized colored bands and lines …

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  • 68DFS 346 — Aircraft 346 P Role Research aircraft Manufacturer …

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  • 69Wallops Flight Facility — (WFF) Airport codes|WAL|KWAL, located on the Eastern Shore of Virginia, is operated by the National Aeronautics and Space Administration’s (NASA) Goddard Space Flight Center primarily as a rocket launch site to support science and exploration… …

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  • 70Gurney flap — The Gurney Flap (or wickerbill) is a small flat tab projecting from the trailing edge of a wing. Typically it is set at a right angle to the pressure side surface of the airfoil,cite journal author = Van Dam, C.P. coauthors = Yen, D.T.; Vijgen, P …

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