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Measured And Calculated Effects Of Angle Of Attack On The Transonic Flutter Of A Supercritical Wing
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Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781725156456 Total Pages :34 pages Book Rating :4.1/5 (564 download)
Book Synopsis Measured and Calculated Effects of Angle of Attack on the Transonic Flutter of a Supercritical Wing by : National Aeronautics and Space Administration (NASA)
Download or read book Measured and Calculated Effects of Angle of Attack on the Transonic Flutter of a Supercritical Wing written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-08-13 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: For abstract see A82-30143. Yates, E. C., Jr. and Wynne, E. C. and Farmer, M. G. Langley Research Center NASA-TM-83276, NAS 1.15:83276 RTOP 505-33-53-07...
Book Synopsis Measured and Calculated Effects of Angle of Attack on the Transonic Flutter of a Supercritical Wing by :
Download or read book Measured and Calculated Effects of Angle of Attack on the Transonic Flutter of a Supercritical Wing written by and published by . This book was released on 1982 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Aeroelastic Effects on the Flutter of a Supercritical Wing by :
Download or read book Static Aeroelastic Effects on the Flutter of a Supercritical Wing written by and published by . This book was released on 1987 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: It is well known that wings with supercritical airfoils generally have lower transonic flutter speeds than similar wings with conventional airfoils and that small increases in angle of attack from zero and the accompanying static aeroelastic deformations have further detrimental effects on transonic flutter. This paper presents results of an effort to calculate the effects of angle of attack and the associated aeroelastic deformation on the flutter of a highly swept supercritical wing (TF-8A) by use of modified strip analysis. The spanwise distributions of steady-state section life-curve slope and aerodynamic calculations for as input for these calculations were obtained from static aeroelastic calculations for the wing by use of hte FL022 transonic code and an assumed dynamic pressure. The process is iterative so that flutter can be obtained at the same dynamic pressure as that used to calculate the statically deformed shape and loading about which the flutter oscillation occurs (matched conditions). Investigation results show that the unconventional backward turn of the transonic dip in the experimental flutter boundary for angles of attack greater than zero is caused by variations in mass ratio and not by static aeroelastic deformation, although inclusion of the latter appears to be required for quantitative accuracy in the calculations. For the very high subsonic Mach numbers of this investigation, quantitative accuracy will also require inclusion of viscous effects on shock strength and location.
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Book Synopsis Effects of Angle of Attack and Thickness Ratio on the Flutter of a Rigid Unswept Diamond-airfoil-section Wing at a Mach Number of 10.0 by : Lou S. Young
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Book Synopsis Prediction of Transonic Flutter for a Supercritical Wing by Modified Strip Analysis and Comparison with Experiment by :
Download or read book Prediction of Transonic Flutter for a Supercritical Wing by Modified Strip Analysis and Comparison with Experiment written by and published by . This book was released on 1981 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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Book Synopsis Government Reports Annual Index: Keyword A-L by :
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Book Synopsis A Numerical Model of Unsteady, Subsonic Aeroelastic Behavior by : Thomas William Strganac
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