Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range 8 ̊to 90 ̊
By: William Bihrle, Jr., Randy S. Hultberg.
Contributors: Bihrle, William.; Hultberg, Randy S.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.; Langley Research Center.
Series: NASA contractor report -- NASA CR-3097.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Branch]
Published: 1979
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Subjects: Spin (Aerodynamics) -- Mathematical models.; Wind tunnel balances.
Notes: Includes bibliographical references.
Table of contents: value: v. 1. High-wing model B; value: v. 2. Low-wing model B.