Control theory based airfoil design using the Euler equations
By: Antony Jameson and James Reuther.
Contributors: Research Institute for Advanced Computer Science (U.S.)
Series: NASA contractor report -- NASA CR-196360.; RIACS technical report -- 94.18.; RIACS technical report -- TR 94-18.
Publisher: Research Institute for Advanced Computer Science, NASA Ames Research Center; National Technical Information Service, distributor
Published: 1994
Place of publication: [Moffett Field, Calif.]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Airfoils.; Control theory.; Drag.; Euler equations of motions.; Finite volume method.; Flow equations.; Potential flow.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0049-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1994] 1 microfiche.