Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8êto 90ê
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 -- 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. 1. Influence of airplane components for model D / J. N. Ralston; value: v. 1. Low-wing model A / Randy S. Hultberg and William Mulcay; value: v. 2. High-wing model A / William Mulcay and Robert Rose; value: v. 3. Effect of wing leading-edge modifications model A / William Bihrle, Jr. and William Mulcay