An Experimental Study Of The Effect Of Pitch Rate On Delta Wing Aerodynamics And Stability
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An Experimental Study of the Effect of Pitch Rate on Delta Wing Aerodynamics and Stability
| Author | : National Aeronautics and Space Administration (NASA) |
| Publisher | : Createspace Independent Publishing Platform |
| Total Pages | : 56 |
| Release | : 2018-07-02 |
| Genre | : |
| ISBN | : 9781722182946 |
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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. Bragg, M. B. Unspecified Center...
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