Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 20
By: John N. Ralston and Billy P. Barnhart ; prepared for Langley Research Center.
Contributors: 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.; NASA contractor report -- NASA CR-3248.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office
Published: 1984
Place of publication: [Washington, D.C.?]
Language: eng
Format: Microform
Subjects: Spin (Aerodynamics) -- Mathematical models.; Wind tunnel balances.
Notes: Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1984]. 4 microfiches ; 11 x 15 cm.

"Bihrle Applied Research, Inc."

Description based on vol. 3.

"Contract NAS1-16205."

"N84-25641"--Microfiche header.

Includes bibliographical references.
Table of contents: title: v. 3. Influence of control deflection on predicted model D spin modes.