Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8j to 90j
By: prepared for Langley Research Center.
Contributors: Ralston, J. N.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.; Langley Research Center.
Series: NASA contractor report -- NASA CR-3246.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1983
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Subjects: Rotational motion (Rigid dynamics); Airplanes -- Wings.; Unsteady flow (Aerodynamics); Wind tunnels -- Flow visualization.; Spin (Aerodynamics)
Notes: Chiefly graphs.

"March 1983"--Cover.

Includes bibliographical references.
Table of contents: value: v. 4. Influence of airplane components for model D / J. N. Ralston.