Approach and landing investigation at lift-drag ratios of 2 to 4 utilizing a straight-wing fighter airplane /
by Gene J. Matranga and Neil A. Armstrong.

Similar Items

• Approach and landing investigation at lift-drag ratios of 3 to 4 utilizing a delta-wing interceptor airplane

  Author

  Matranga, Gene J.

  Published

  1959

• Analysis of X-15 landing approach and flare characteristics determined from the first 30 flights

  Author

  Matranga, Gene J.

  Published

  1961

• Launch characteristics of the X-15 research airplane as determined in flight

  Author

  Matranga, Gene J.

  Published

  1961

• Launch, low-speed, and landing characteristics determined from the first flight of the North American X-15 research airplane

  Author

  Finch, Thomas W.

  Published

  1959

• Design and operational characteristics of a lunar-landing research vehicle

  Author

  Bellman, Donald R.

  Published

  1965

• Utilization of a fixed-base simulator to study the stall and spin characteristics of fighter airplanes

  Author

  Moore, Frederick L.

  Published

  1971

• Investigation of an automatic spin-prevention system for fighter airplanes

  Author

  Gilbert, William P.

  Published

  1972

• Flight and simulation investigation of methods for implementing noise-abatement landing approaches

  Author

  Quigley, Hervey C.

  Published

  1970

• Flight investigation of the low-speed characteristics of a 45⁰ swept-wing fighter-type airplane with blowing boundary-layer control applied to the leading- and trailing-edge flaps

  Author

  Quigley, Hervey C.

  Published

  1960

• Low-lift-to-drag-ratio approach and landing studies using a CV-990 airplane

  Author

  Kock, Berwin M.

  Published

  1972