An assessment of the capability to calculate tilting prop-rotor aircraft performance, loads, and stability
By: Wayne Johnson
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Series: NASA technical paper -- 2291
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1984
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 19
Subjects: Vertically rising aircraft; Rotors (Helicopters); Vibration (Aeronautics); Stability of helicopters
Notes: "March 1984"--Cover

Distributed to depository libraries in microfiche

Includes bibliographical references