Predictions of F-111 TACT aircraft buffet response and correlations of fluctuating pressures measured on aluminum and steel models and the aircraft
By: prepared for Ames Research Center, Dryden Flight Research Facility.
Contributors: Cunningham, Atlee M.; Coe Engineering, Inc; Dryden Flight Research Facility
Publisher: NASA
Published: 1987
Place of publication: Washington
Number of pages: 148
Subjects: Buffeting; Damping
Notes: Bibliography: p.34-35.