Unsteady, transonic flow around delta wings undergoing coupled and natural modes response
Subtitle: a multidisciplinary problem
By: by Margaret Anne Menzies ; a dissertation submitted to the Faculty of Old Dominion University in partial fulfillment of the requirement for the degree of Doctor of Philosphy, Aerospace Engineering, Old Dominion University.
Contributors: United States. National Aeronautics and Space Administration.
Series: [NASA contractor report] -- NASA-CR-203248.
Publisher: Old Dominion University; National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1996
Place of publication: [Norfolk, VA; Washington, D.C; Springfield, Va
Language: eng
Subjects: Transonic flow.; Unsteady flow.; Delta wings.; Aerodynamic coefficients.; Navier-Stokes equation.; Angle of attack.; Flow distribution.; Flow equations.; Swept wings.; Leading edges.
Notes: Shipping list no.: 98-1104-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.