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Investigation Of Flutter Characteristics Of Four Series Of Low Aspect Ratio Surfaces At Mach Numbers From 149 To 287
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Book Synopsis Investigation of Flutter Characteristics of Four Series of Low-aspect-ratio Surfaces at Mach Numbers from 1.49 to 2.87 by : Robert V. Jr Doggett
Download or read book Investigation of Flutter Characteristics of Four Series of Low-aspect-ratio Surfaces at Mach Numbers from 1.49 to 2.87 written by Robert V. Jr Doggett and published by . This book was released on 1961 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of Flutter Characteristics of Three Low-aspect-ratio All-movable Half-span Control Surfaces at Mach Numbers from 1.49 to 2.87 by : Homer G. Morgan
Download or read book Investigation of Flutter Characteristics of Three Low-aspect-ratio All-movable Half-span Control Surfaces at Mach Numbers from 1.49 to 2.87 written by Homer G. Morgan and published by . This book was released on 1958 with total page 35 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Flutter Characteristics of an Aspect-ratio-4, 45° Sweptback, Taper-ratio-0.2 Plan Form by : John R. Unangst
Download or read book Transonic Flutter Characteristics of an Aspect-ratio-4, 45° Sweptback, Taper-ratio-0.2 Plan Form written by John R. Unangst and published by . This book was released on 1959 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Some Low-speed Flutter Characteristics of Simple Low-aspect-ratio Delta Wing Models by : Robert V. Doggett (Jr)
Download or read book Some Low-speed Flutter Characteristics of Simple Low-aspect-ratio Delta Wing Models written by Robert V. Doggett (Jr) and published by . This book was released on 1989 with total page 11 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flutter Investigation of Two Thin, Low-aspect-ratio, Swept, Solid, Metal Wings in the Transonic Range by Use of Free-falling Body by : W. T. Lauten
Download or read book Flutter Investigation of Two Thin, Low-aspect-ratio, Swept, Solid, Metal Wings in the Transonic Range by Use of Free-falling Body written by W. T. Lauten and published by . This book was released on 1952 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Some Effects of Sweep and Aspect Ratio on the Transonic Flutter Characteristics of a Series of Thin Cantilever Wings Having a Taper Ratio of 0.6 by : John R. Unangst
Download or read book Some Effects of Sweep and Aspect Ratio on the Transonic Flutter Characteristics of a Series of Thin Cantilever Wings Having a Taper Ratio of 0.6 written by John R. Unangst and published by . This book was released on 1963 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flutter at Very High Speeds by : Harry L. Runyan
Download or read book Flutter at Very High Speeds written by Harry L. Runyan and published by . This book was released on 1957 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt: This paper is concerned with a discussion of some of the problems of flutter and aeroelasticity that are or may be important at high speeds. Various theoretical procedures for treating high Mach number flutter are reviewed. Application of two of these methods, namely, the Van Dyke method and piston-theory method, is made to a specific example and compared with linear two- and three-dimensional results. It is shown that the effects of thickness and airfoil shape are destabilizing as compared with linear theory at high Mach number. In order to demonstrate the validity of these large predicted effects, experimental flutter results are shown for two rectangular wings at Mach numbers of 6.86 and 3. The results of nonlinear piston-theory calculations were in good agreement with experiment, whereas the results of using two- and three-dimensional linear theory were not. In addition, some results demonstrating the importance of including camber modes in a flutter analysis are shown, as well as a discussion of one case of flutter due to aerodynamic heating.
Book Synopsis An experimental investigation on transonic flutter characteristics of low aspect-ratio sweptback all-moving horizontal tail surface models by : Eiichi Nakai
Download or read book An experimental investigation on transonic flutter characteristics of low aspect-ratio sweptback all-moving horizontal tail surface models written by Eiichi Nakai and published by . This book was released on 1981 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Flutter Investigation of a Cantilevered, Aspect-ratio-4, 45 Degree Sweptback, Untapered Wing with Three Different Pylon-mounted External Store Configurations by : Charles L. Ruhlin
Download or read book Transonic Flutter Investigation of a Cantilevered, Aspect-ratio-4, 45 Degree Sweptback, Untapered Wing with Three Different Pylon-mounted External Store Configurations written by Charles L. Ruhlin and published by . This book was released on 1957 with total page 35 pages. Available in PDF, EPUB and Kindle. Book excerpt: A brief, exploratory investigation has been made of the transonic flutter characteristics of a cantilevered, aspect-ratio-4, 45 degree sweptback, untapered wing with three different pylon-mounted external-store configuration. For stores located near the midsemispan and weighing about 0.7 of the semispan wing, the flutter speed was not changed when the store center of gravity was moved from 38 to 12 percent of the chord. The flutter speeds for these two stores were from 14 to 19 percent less than those obtained with the wings alone at subsonic speeds. The rate of rise of flutter speed with Mach number in the low supersonic range was about the same for the wing with stores as for the plain wing.
Book Synopsis Basic Principles of the Indicial Lifting-surface Flutter-analysis Procedure by : Bernard Mazelsky
Download or read book Basic Principles of the Indicial Lifting-surface Flutter-analysis Procedure written by Bernard Mazelsky and published by . This book was released on 1962 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method of flutter analysis utilizing indicial functions to represent the unsteady aerodynamics is described. Basic concepts are illustrated for a two-dimensional wing; the extension to a spanwise distorting wing is also discussed. Significant aerodynamic parameters pertinent to a highly swept, hypersonic delta wing are reviewed. For these wings the principal factor for adequate prediction of flutter is determination of the steady and quasi-steady aerodynamic influence coefficients. The unsteady contributions are shown to have a negligible effect on the flutter characteristics.
Book Synopsis A Study of Several Factors Affecting the Flutter Characteristics Calculated for Two Swept Wings by Piston Theory and by Quasi-steady Second-order Theory and Comparison with Experiments by : Robert Merrill Bennett
Download or read book A Study of Several Factors Affecting the Flutter Characteristics Calculated for Two Swept Wings by Piston Theory and by Quasi-steady Second-order Theory and Comparison with Experiments written by Robert Merrill Bennett and published by . This book was released on 1963 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flutter of a Low-aspect-ratio Rectangular Wing by : Stanley R. Cole
Download or read book Flutter of a Low-aspect-ratio Rectangular Wing written by Stanley R. Cole and published by . This book was released on 1989 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Study of the Effect of Rearward Mounted Heavy Nacelles on the Flutter Characteristics of Low-aspect-ratio Wings at Transonic and Supersonic Speeds by : G. M. Levey
Download or read book An Experimental Study of the Effect of Rearward Mounted Heavy Nacelles on the Flutter Characteristics of Low-aspect-ratio Wings at Transonic and Supersonic Speeds written by G. M. Levey and published by . This book was released on 1961 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Flutter Characteristics of Low Aspect Ratio Wings in Incompressible Flow by : Herbert R. Lawrence
Download or read book The Flutter Characteristics of Low Aspect Ratio Wings in Incompressible Flow written by Herbert R. Lawrence and published by . This book was released on 1954 with total page 27 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flight Stability and Automatic Control by : Robert C. Nelson
Download or read book Flight Stability and Automatic Control written by Robert C. Nelson and published by WCB/McGraw-Hill. This book was released on 1998 with total page 441 pages. Available in PDF, EPUB and Kindle. Book excerpt: The second edition of Flight Stability and Automatic Control presents an organized introduction to the useful and relevant topics necessary for a flight stability and controls course. Not only is this text presented at the appropriate mathematical level, it also features standard terminology and nomenclature, along with expanded coverage of classical control theory, autopilot designs, and modern control theory. Through the use of extensive examples, problems, and historical notes, author Robert Nelson develops a concise and vital text for aircraft flight stability and control or flight dynamics courses.
Download or read book The Aeronautical Journal written by and published by . This book was released on 1981 with total page 554 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aeronautical Enginnering: A Cumulative Index to a Continuing Bibliography (supplement 312) by :
Download or read book Aeronautical Enginnering: A Cumulative Index to a Continuing Bibliography (supplement 312) written by and published by . This book was released on 1994 with total page 392 pages. Available in PDF, EPUB and Kindle. Book excerpt:
