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Hypersonic Flutter Model Tests Of Advanced Wing Configurations At Initial Angles Of Attack
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Book Synopsis Hypersonic Flutter Model Tests of Advanced Wing Configurations at Initial Angles of Attack by :
Download or read book Hypersonic Flutter Model Tests of Advanced Wing Configurations at Initial Angles of Attack written by and published by . This book was released on 1964 with total page 210 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report presents an experimental and analytical flutter investigation of a low aspect ratio lifting surface with a 70 degree leading edge sweep angle, and thickness ratios of 3%, 6%, and 9% in the hypersonic speed range from M = 5.0 to M = 8.0. The 6% thickness ratio models were tested at uncoupled frequency ratios of 0.60, 0.75, and 0.90. The models used were of the semirigid type with a double wedge leading edge to 15% chord with constant thickness from the 15% chord to a blunt trailing edge. All experimental flutter configurations were analyzed using an analog representation of a quasi-steady flutter solution. The aerodynamic representations investigated were experimentally obtained static aerodynamic force coefficients and aerodynamic force coefficients derived from steady-state, two-dimensional, shock-expansion techniques with sweep angle corrections. The relative effect on the flutter characteristics of inclusion of piston theory derived rate terms in the aerodynamics was investigated for configurations.
Book Synopsis Flutter Model Tests of Advanced Wing Configurations at Initial Angles of Attack by : D. A. Brown
Download or read book Flutter Model Tests of Advanced Wing Configurations at Initial Angles of Attack written by D. A. Brown and published by . This book was released on 1964 with total page 127 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report describes an experimental and analytical program conducted to determine the transonic and supersonic flutter boundary of a highly swept, low aspect ratio lifting surface typical of re-entry vehicle configurations. Several semi-rigid flutter models were constructed and tested at Mach numbers from .4 to 1.2 and also at Mach numbers from 2.0 to 5.0. The effects on flutter speed of initial angle of attack, un-coupled frequency ratio, model thickness ratio and a tip surface normal to the plane of the basic model were determined. The model aspect ratio was .889, the leading edge sweep angle was 70 degrees and the thickness ratio of the basic model was 6%. Other thicknesses were 3% and 9%. The cross-section of the model was modified wedge having a wedge angle in the streamwise direction of 22 degrees 38 minutes. The trailing edge was blunt. (Author).
Book Synopsis Hypersonic Flutter Analysis Using Measured Static Aerodynamic Derivatives, and Comparison with Experiment by : Robert C. Goetz
Download or read book Hypersonic Flutter Analysis Using Measured Static Aerodynamic Derivatives, and Comparison with Experiment written by Robert C. Goetz and published by . This book was released on 1969 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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Book Synopsis Proceedings of Symposium on Aeroelastic & Dynamic Modeling Technology, 23-24-25 September 1963, Dayton, Ohio by :
Download or read book Proceedings of Symposium on Aeroelastic & Dynamic Modeling Technology, 23-24-25 September 1963, Dayton, Ohio written by and published by . This book was released on 1964 with total page 800 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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Book Synopsis Hypersonic Wing Test Structure Design, Analysis, and Fabrication by :
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Book Synopsis Aeronautics and Space Report of the President by : United States. President
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Book Synopsis Aeronautics and Space Report of the President by : United States. President (1981-1989 : Reagan)
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