The benchmark aeroelastic models program: Description and highlights of initial results
The benchmark aeroelastic models program: Description and highlights of initial results
- Neue Suche nach: Bennett, Robert M.
- Neue Suche nach: Eckstrom, Clinton V.
- Neue Suche nach: Rivera, Jose A., Jr.
- Neue Suche nach: Dansberry, Bryan E.
- Neue Suche nach: Farmer, Moses G.
- Neue Suche nach: Durham, Michael H.
- Neue Suche nach: Bennett, Robert M.
- Neue Suche nach: Eckstrom, Clinton V.
- Neue Suche nach: Rivera, Jose A., Jr.
- Neue Suche nach: Dansberry, Bryan E.
- Neue Suche nach: Farmer, Moses G.
- Neue Suche nach: Durham, Michael H.
An experimental effort was implemented in aeroelasticity called the Benchmark Models Program. The primary purpose of this program is to provide the necessary data to evaluate computational fluid dynamic codes for aeroelastic analysis. It also focuses on increasing the understanding of the physics of unsteady flows and providing data for empirical design. An overview is given of this program and some results obtained in the initial tests are highlighted. The tests that were completed include measurement of unsteady pressures during flutter of rigid wing with a NACA 0012 airfoil section and dynamic response measurements of a flexible rectangular wing with a thick circular arc airfoil undergoing shock boundary layer oscillations.
Dokumentinformationen
The benchmark aeroelastic models program: Description and highlights of initial results
AGARD Structures and Materials Panel Specialists'' Meeting on Transonic Unsteady Aerodynamics and Aeroelasticity ; 1991 ; San Diego, CA, United States
1991-12-01
Aufsatz (Konferenz)
Keine Angabe
Englisch