Identification of aircraft stability derivatives for the high angle-of-attack regime
By: prepared for Office of Naval Research.
Contributors: Systems Control Inc; U.S. Office of Naval Research
Publisher: Systems Control Inc
Published: 1972
Place of publication: Palo Alto, Calif
Number of pages: 194
Subjects: Aircraft spin; Angle of attack; Flight simulation; Stability derivatives; Stalling
Notes: Technical report #1.

Bibliographical references: p.136-139.