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.


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    Title :

    An experimental study of the effect of pitch rate on delta wing aerodynamics and stability


    Contributors:

    Publication date :

    1988-08-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :