Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8t̊o 90 ̊
By: prepared for Langley Research Center under contract NAS1-14849.
Contributors: Hultberg, Randy S.; Mulcay, William.; Rose, Robert A.; Bihrle, William.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.; Langley Research Center.
Series: NASA contractor report -- NASA CR-3100, 3101, 3102.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; For sale by the National Technical Information Service]
Published: 1979
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Subjects: Aerodynamics.; Spin (Aerodynamics) -- Mathematical models.; Flight simulators.
Notes: "Scientific and Technical Information Branch"--Vol. 2., t.p.

Vol. 1 dated 1980.

Vol. 3 title differs.

Includes bibliographical references.
Table of contents: 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.