Experimental Study of the Effect of Pitch Rate on Delta Wing Aerodynamics and Stability. Final Report, April 1, 1986-June 30, 1988

摘要

The final report for the research conducted under this grant (NAG1-641) are contained in the two documents attached as Apendices A and B. The first is the presentation made to NASA Langley personnel on 10 December, 1987, which gave a brief analysis of the experiments. The second is a copy of an AIAA paper given in June 1988, which describes in detail the test setup, data acquisition and reduction, and results obtained.