Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range 8ê to 90ê
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 -- 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