Download or read book Theoretical Estimation of the Transonic Aerodynamic Characteristics of a Supercritical Wing Transport Model with Trailing Edge Controls 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 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method for rapidly estimating the overall forces and moments at supercritical speeds, below drag divergence, of transport configurations with supercritical wings is presented. The method was also used for estimating the rolling moments due to the deflection of wing trailing-edge controls. This analysis was based on a vortex-lattice technique modified to approximate the effects of wing thickness and boundary-layer induced camber. Comparisons between the results of this method and experiment indicate reasonably good correlation of the lift, pitching moment, and rolling moment. The method required much less storage and run time to compute solutions over an angle-of-attack range than presently available transonic nonlinear methods require for a single angle-of-attack solution. Luckring, J. M. and Mann, M. J. Langley Research Center NASA-TP-1253, L-11257 RTOP 505-11-16-07...
Download or read book Theoretical Estimation of the Transonic Aerodynamic Characteristics of a Supercritical wing Transport Model with Trailing edge Controls written by James M. Luckring and published by . This book was released on 1978 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Transonic Aerodynamic Characteristics of a Supercritical wing Transport Model with Trailing edge Controls written by Michael J. Mann and published by . This book was released on 1977 with total page 348 pages. Available in PDF, EPUB and Kindle. Book excerpt: The effects of wing trailing-edge control surfaces on the static transonic aerodynamic characteristics of a transport configuration with a supercritical wing were studied. The configuration was tested with both an area-ruled fuselage and a cylindrical fuselage. The Mach number range was from 0.80 to 0.96 and the angle of attack range was from -1 deg to 12 deg. The Reynolds number was 1,580,000 based on the mean aerodynamic chord. Tabular data are presented.
Download or read book Theoretical Estimation of the Transonic Aerodynamic Characteristics of a Supercritical wing Transport Model with Trailing edge Controls written by James M. Luckring and published by . This book was released on 1978 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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Download or read book Transonic Aerodynamics Characteristics of a Supercritical wing Transport Model with Trailing edge Controls written by Michael J. Mann and published by . This book was released on 1977 with total page 336 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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