The final report for the research conducted under this grant (NAG1-641) are contained in the two documents attached as Appendices 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.
Experimental Study of the Effect of Pitch Rate on Delta Wing Aerodynamics and Stability. Final Report, April 1, 1986-June 30, 1988
1988
55 pages
Report
Keine Angabe
Englisch