Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds
By: Jack Nugent and Odis C. Pendergraft.
Contributors: Pendergraft, Odis C.; Ames Research Center
Publisher: Ames Research Center
Published: 1987
Place of publication: Edwards, Calif
Number of pages: 120
Subjects: Afterbodies; Nozzle flow
Notes: Bibliographical references: p.26.