Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 20⁰ to 90⁰
By: prepared for Langley Research Center
Contributors: Ralston, J. N; Barnhart, Billy; Langley Research Center; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office; Bihrle Applied Research, Inc
Series: NASA contractor report -- 3248
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; National Technical Information Service]
Published: 1984
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Subjects: Spin (Aerodynamics) -- Mathematical models; Wind tunnel balances
Notes: "Bihrle Applied Research, Inc."

"June 1984"--Cover

NAS1-16205
Table of contents: value: v. 3. Influence of control deflection on predicted model D spin modes / John N. Ralston and Billy P. Barnhart