Prediction of wind tunnel effects on the installed F/A-18A inlet flow field at high angles-of-attack
By: Crawford F. Smith.
Contributors: United States. National Aeronautics and Space Administration.
Series: NASA contractor report -- 195429.; NASA contractor report -- NASA CR-195429.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1995
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Air flow.; Angle of attack.; Engine inlets.; F-18 aircraft.; Flow distribution.; Inlet flow.; Intake systems.; Wind tunnel tests.; Wind tunnel walls.; Wind tunnels.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0419-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.