Design guide for pitch-up evaluation and investigation at high subsonic speeds of possible limitations due to wing-aspect-ratio variations - Spreemann, Kenneth P.; United States. National Aeronautics and Space Administration (Washington [D.C.] : National Aeronautics and Space Administration, 1959)
"August 1959."
Cover title.
Includes bibliographical references (p. 14-16).
Mode of access: Internet.
Keywords: Airplanes, Tailless; Airplanes -- Tail surfaces; Aspect ratio (Aerofoils); Pitching (Aerodynamics); Airplanes -- Wings -- Design and construction