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  • 1
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    Performance characteristics of the lifting body vehicle (1970)
    In:  CASI
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    Publication Date: 2005-08-18
    Description: Prediction of performance characteristics for lifting body vehicle
    Keywords: SPACE VEHICLES
    Type: FLIGHT TEST RESULTS PERTAINING TO THE SPACE SHUTTLECRAFT OCT. 1970; P 43-58
    Format: text
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    NASA TECHNICAL REPORTS
  • 2
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    A comparison of two methods of extracting stability derivatives from flight test data (1974)
    In:  Other Sources
    Details
    Publication Date: 2011-08-16
    Description: Two methods for extracting stability derivatives from flight data are compared. A modified Newton-Raphson quasilinearization minimization technique and a digital-analog (hybrid) matching technique were used to analyze the same data maneuvers obtained from two aircraft. About 70 maneuvers from an F-111E aircraft were analyzed over a Mach number range of 0.3 to 2.0 and an angle of attack range of 3 to 19 degrees. About 20 maneuvers were analyzed for the X-24A lifting body at Mach numbers of 0.5, 0.8, and 0.9, and an angle of attack range of 4 to 13 degrees. Stability derivatives were extracted from these maneuvers and the results from the two techniques, along with wind tunnel results, were compared.
    Keywords: AERODYNAMICS
    Type: NASA. Flight Res. Center Parameter Estimation Tech. and Appl. in Aircraft Flight Testing; p 43-48
    Format: text
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    NASA TECHNICAL REPORTS
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