Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane

Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane /

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Bibliographic Details
Main Author: Allison, Dennis O.
Corporate Author: Langley Research Center
Other Authors: Sewall, William G.
Format: Government Document Book
Language:English
Published: Hampton, Va. : Springfield, VA : National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service (NTIS) [distributor], [1995]
Series:NASA technical paper 3516.
Subjects:
Aircraft models.
Airfoils.
Leading edges.
Maneuverability.
Pressure distribution.
Subsonic speed.
Trailing edges.
Transonic speed.
Wind tunnel tests.
Wing-fuselage stores.

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