Publication Date:
2004-12-03
Description:
The work to be described was performed at the NASA Langley UPWT (4-ft supersonic), test section #2, during 21-24 May 1996. The configuration being tested was the 1.675% Ref H controls model; test conditions were Ma = 2.40, Re = 3 million/ft. This was an exploration of a new technique, and it was not intended to provide definitive comparison of measured and computed skin friction results. It is, however, hoped that the experience gained will make such a rigorous comparison possible in the future.
Keywords:
Aerodynamics
Type:
1997 NASA High-Speed Research Program Aerodynamic Performance; Volume 1; Part 2; 1478-1499; NASA/CP-1999-209691/VOL1/PT2
Format:
text