Clinton V. Eckstrom

Measurements of unsteady pressure and structural response for an elastic supercritical wing

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Author

Clinton V. Eckstrom

Contributions

Seidel, David A. - Contributor
Sandford, M. C. - Contributor
Langley Research Center. - Contributor

Publication

1994 - National Aeronautics and Space Administration, Langley Research Center, Hampton, Va, Virginia

Language

English

Word Count

0 words, Guess

Page Count

0 pages

Physical Format

Microform

Identifiers

OCLC Control Number32863973
Open LibraryOL17790670M

Subjects

Topics

Unsteady flow Aeroelasticity Transonic speed Dynamic response Wind tunnel tests Supercritical wings Pressure distribution

Series Statement

NASA technical paper -- 3443.

Other Editions

Measurements of unsteady pressure and structural response for an elastic supercritical wingMicroformNational Aeronautics and Space Administration, Langley Research Center1994

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