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Author : Ta Li
Publisher :
ISBN 13 :
Total Pages : 46 pages
Book Rating : 4.:/5 (977 download)
Download or read book Aerodynamic Influence Coefficients for an Oscillating Finite Thin Wing in Supersonic Flow written by Ta Li and published by . This book was released on 1956 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Robert W. Warner
Publisher :
ISBN 13 :
Total Pages : 72 pages
Book Rating : 4.:/5 (31 download)
Download or read book A Method for Calculating the Aerodynamic Forces Due to Arbitrary, Time Dependent Downwash for a Class of Thin, Flexible Wings at Supersonic Speeds written by Robert W. Warner and published by . This book was released on 1960 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 708 pages
Book Rating : 4.:/5 (319 download)
Download or read book NASA Technical Note written by and published by . This book was released on 1971 with total page 708 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Robert W. Warner
Publisher :
ISBN 13 :
Total Pages : 74 pages
Book Rating : 4.:/5 (317 download)
Download or read book A Method for Calculating the Aerodynamic Forces Due to Arbitrary, Time-dependent Downwash for a Class of Thin, Flexible Wings at Supersonic Speeds written by Robert W. Warner and published by . This book was released on 1960 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Allen F. Donovan
Publisher : Princeton University Press
ISBN 13 : 1400879906
Total Pages : 863 pages
Book Rating : 4.4/5 (8 download)
Download or read book Aerodynamic Components of Aircraft at High Speeds written by Allen F. Donovan and published by Princeton University Press. This book was released on 2015-12-08 with total page 863 pages. Available in PDF, EPUB and Kindle. Book excerpt: Volume VII of the High Speed Aerodynamics and Jet Propulsion series. It deals with applications to specific components of the complete aircraft. Sections of the volume include: aerodynamics of wings at high speed, aerodynamics of bodies at high speed, interaction problems, propellers at high speed, diffusers and nozzles, and nonsteady wing characteristics. Originally published in 1957. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.
Author : Elie Carafoli
Publisher : Pergamon
ISBN 13 :
Total Pages : 618 pages
Book Rating : 4.:/5 (89 download)
Download or read book Wing Theory in Supersonic Flow written by Elie Carafoli and published by Pergamon. This book was released on 1969 with total page 618 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Edward Carson Yates
Publisher :
ISBN 13 :
Total Pages : 62 pages
Book Rating : 4.:/5 (31 download)
Download or read book Comparative Evaluation of Methods for Predicting Flutter and Divergence of Unswept Wings of Finite Span written by Edward Carson Yates and published by . This book was released on 1963 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : United States. Wright Air Development Division
Publisher :
ISBN 13 :
Total Pages : 1268 pages
Book Rating : 4.3/5 (91 download)
Download or read book WADC Technical Report written by United States. Wright Air Development Division and published by . This book was released on 1957 with total page 1268 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Valter J. E. Stark
Publisher :
ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.E/5 ( download)
Download or read book Calculation of Lifting Forces on Oscillating Wings written by Valter J. E. Stark and published by . This book was released on 1964 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 528 pages
Book Rating : 4.:/5 (31 download)
Download or read book Proceedings of NASA Conference on Supersonic-Transport Feasibility Studies and Supporting Research, September 17-19, 1963, Langley Research Center, Langley Station, Hampton, Va written by and published by . This book was released on 1963 with total page 528 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Raymond L. Bisplinghoff
Publisher : Courier Corporation
ISBN 13 : 0486783162
Total Pages : 545 pages
Book Rating : 4.4/5 (867 download)
Download or read book Principles of Aeroelasticity written by Raymond L. Bisplinghoff and published by Courier Corporation. This book was released on 2013-10-17 with total page 545 pages. Available in PDF, EPUB and Kindle. Book excerpt: Geared toward professional engineers, this volume will be helpful for students, too. Topics include methods of constructing static and dynamic equations, heated elastic solids, forms of aerodynamic operators, structural operators, and more. 1962 edition.
Author : Alfredo Navarro Crespo
Publisher :
ISBN 13 :
Total Pages : 84 pages
Book Rating : 4.:/5 (31 download)
Download or read book Development of Three-dimensional Pressure-distribution Functions for Lifting Surfaces with Trailing-edge Controls Based on the Integral Equation for Subsonic Flow written by Alfredo Navarro Crespo and published by . This book was released on 1969 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt: Three dimensional pressure distribution functions for lifting surfaces with trailing-edge controls based on integral equations for subsonic flow.
Author : Jieqian Zhang
Publisher :
ISBN 13 :
Total Pages : 76 pages
Book Rating : 4.:/5 (249 download)
Download or read book The Aerodynamic Behavior of a Harmonically Oscillating Finite Sweptback Wing in Supersonic Flow written by Jieqian Zhang and published by . This book was released on 1951 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt: By an extension of Evvard's "diaphragm" concept outside the wing tip, two approximate methods are presented for calculating the aerodynamic behavior of harmonically oscillating, sweptback finite wings with both supersonic leading and trailing edges - one expressing the integration in terms of Fresnal integrals and the second one similar to the first except that a series of expansion of the source-strength function is used. If the wing frequency parameter is small both methods give accurate results in the engineering sense without requiring undue computing skill. A number of graphs are presented to show pressure distribution of the wings at different Mach numbers, sweepback angles, and frequency parameters. Comparisons of pressure coefficients calculated from present methods and exact two dimensional solutions based on linearized theory are made.
Author : Patrick A. Gainer
Publisher :
ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.:/5 (31 download)
Download or read book A Method of Determining Aerodynamic-influence Coefficients from Wind-tunnel Data for Wings at Supersonic Speeds written by Patrick A. Gainer and published by . This book was released on 1961 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 404 pages
Book Rating : 4.F/5 ( download)
Download or read book Aerodynamic Inputs for Problems in Aircraft Dynamics written by and published by . This book was released on 1977 with total page 404 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Floyd V. Bennett
Publisher :
ISBN 13 :
Total Pages : 48 pages
Book Rating : 4.:/5 (31 download)
Download or read book Comparison of Experimental and Theoretical Static Aeroelastic Loads and Deflections of a Thin 45° Wing in Supersonic Flow written by Floyd V. Bennett and published by . This book was released on 1961 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt: Wind tunnel tests showing the effects of static aeroelasticity for a thin 45° delta wing in supersonic flow are presented and compared with theory in the Mach number range 1.30 t o 4.00. Calculated deformations, normal-force coefficients, and pitching-moment coefficients based on a linearized potential theory for subsonic leading edges at a Mach number of 1.30 and a linearized potential theory for supersonic leading edges at Mach numbers of 1.64, 3.00, and 4.00 are shown to compare favorably with the wind-tunnel results.
Author :
Publisher :
ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.:/5 (227 download)
Download or read book A Computer Program for Calculating the Steady and Oscillatory Supersonic Flow Over Thin Wings written by and published by . This book was released on 1985 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: A computer program for the calculation of linearized steady and oscillatory supersonic flow over thin wings has been implemented on an ELXSI. The program uses an explicit finite difference scheme on a characteristic grid to solve for the reduce potential and pressure coefficient on the wing surface. Keywords; Supersonic flow; Thin wings; Computer programs; and Australia.
