Measurements of unsteady pressure and structural response for an elastic supercritical wing
By: Clinton V. Eckstrom, David A. Seidel, and Maynard C. Sandford.
Contributors: Seidel, David A.; Sandford, M. C.; Langley Research Center.
Series: NASA technical paper -- 3443.
Publisher: National Aeronautics and Space Administration, Langley Research Center; For sale by the National Technical Information Service
Published: 1994
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aeroelasticity.; Dynamic response.; Pressure distribution.; Supercritical wings.; Transonic speed.; Unsteady flow.; Wind tunnel tests.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0297-M.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration, 1995] 2 microfiches.