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Some Effects Of Variations In Density And Aerodynamic Parameters On The Calculated Flutter Characteristics Of Finite Span Swept And Unswept Wings At Subsonic And Supersonic Speeds
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Book Synopsis Some Effects of Variations in Density and Aerodynamic Parameters on the Calculated Flutter Characteristics of Finite-span Swept and Unswept Wings at Subsonic and Supersonic Speeds by : Edward Carson Yates
Download or read book Some Effects of Variations in Density and Aerodynamic Parameters on the Calculated Flutter Characteristics of Finite-span Swept and Unswept Wings at Subsonic and Supersonic Speeds written by Edward Carson Yates and published by . This book was released on 1960 with total page 134 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Some Effects of Variations in Density and Aerodynamic Parameters on Calculated Flutter Characteristics of Finite-span Swept and Unswept Wings at Subsonic Speeds [with List of References] by :
Download or read book Some Effects of Variations in Density and Aerodynamic Parameters on Calculated Flutter Characteristics of Finite-span Swept and Unswept Wings at Subsonic Speeds [with List of References] written by and published by . This book was released on 1960 with total page 130 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Note written by and published by . This book was released on 1967 with total page 544 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Use of Experimental Steady-flow Aerodynamic Parameters in the Calculation of Flutter Characteristics for Finite-span Swept Or Unswept Wings at Subsonic, Transonic, and Supersonic Speed by : Edward Carson Yates
Download or read book Use of Experimental Steady-flow Aerodynamic Parameters in the Calculation of Flutter Characteristics for Finite-span Swept Or Unswept Wings at Subsonic, Transonic, and Supersonic Speed written by Edward Carson Yates and published by . This book was released on 1960 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1963 with total page 192 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic and Supersonic Flutter Trend Investigation of a Variable-sweep Wing by : John C. Stonesifer
Download or read book Transonic and Supersonic Flutter Trend Investigation of a Variable-sweep Wing written by John C. Stonesifer and published by . This book was released on 1961 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Monthly Catalog of United States Government Publications by :
Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 1962 with total page 1990 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis U.S. Government Research Reports by :
Download or read book U.S. Government Research Reports written by and published by . This book was released on 1963 with total page 130 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Flutter by : Isadore Edward Garrick
Download or read book Aerodynamic Flutter written by Isadore Edward Garrick and published by . This book was released on 1969 with total page 144 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Use of Aerodynamic Parameters from Nonlinear Theory in Modified-strip-analysis Flutter Calculations for Finite-span Wings at Supersonic Speeds by : Edward Carson Yates
Download or read book Use of Aerodynamic Parameters from Nonlinear Theory in Modified-strip-analysis Flutter Calculations for Finite-span Wings at Supersonic Speeds written by Edward Carson Yates and published by . This book was released on 1963 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Measured and Calculated Subsonic and Transonic Flutter Characteristics of a 45 ̊sweptback Wing Planform in Air and in Freon-12 in the Langley Transonic Dynamics Tunnel by : Edward Carson Yates
Download or read book Measured and Calculated Subsonic and Transonic Flutter Characteristics of a 45 ̊sweptback Wing Planform in Air and in Freon-12 in the Langley Transonic Dynamics Tunnel written by Edward Carson Yates and published by . This book was released on 1963 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low-subsonic Measurements of Static and Dynamic Stability Derivatives of Six Flat-plate Wings Having Leading-edge Sweep Angles of 70 ̊to 84 ̊ by : Robert E. Shanks
Download or read book Low-subsonic Measurements of Static and Dynamic Stability Derivatives of Six Flat-plate Wings Having Leading-edge Sweep Angles of 70 ̊to 84 ̊ written by Robert E. Shanks and published by . This book was released on 1963 with total page 822 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Keywords Index to U.S. Government Technical Reports by :
Download or read book Keywords Index to U.S. Government Technical Reports written by and published by . This book was released on 1963-06-15 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :United States. Department of Commerce. Office of Technical Services Publisher : ISBN 13 : Total Pages :618 pages Book Rating :4.3/5 (91 download)
Book Synopsis Keywords Index to U.S. Government Technical Reports (permuted Title Index). by : United States. Department of Commerce. Office of Technical Services
Download or read book Keywords Index to U.S. Government Technical Reports (permuted Title Index). written by United States. Department of Commerce. Office of Technical Services and published by . This book was released on 1963 with total page 618 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Subsonic and Supersonic Flutter Analysis of a Highly Tapered Swept-wing Planform, Including Effects of Density Variation and Finite Wing Thickness, and Comparison with Experiments by : E. Carson Yates (Jr.)
Download or read book Subsonic and Supersonic Flutter Analysis of a Highly Tapered Swept-wing Planform, Including Effects of Density Variation and Finite Wing Thickness, and Comparison with Experiments written by E. Carson Yates (Jr.) and published by . This book was released on 1967 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt: The flutter characteristics of several wings with an aspect-ratio of 4.0, a taper ratio of 0.2, and a quarter-chord sweepback of 45 deg. have been investigated analytically for Mach numbers up to 2.0. The calculations were based on the modified-strip-analysis method, the subsonic-kernel-function method, piston theory, and quasi-steady second-order theory. Results of t h e analysis and comparisons with experiment indicated that: (1) Flutter speeds were accurately predicted by the modified strip analysis, although accuracy at t h e highest Mach numbers required the use of nonlinear aerodynamic theory (which accounts for effects of wing thickness) for the calculation of the aerodynamic parameters. (2) An abrupt increase of flutter-speed coefficient with increasing Mach number, observed experimentally in the transonic range, was also indicated by the modified strip analysis. (3) In the low supersonic range for some densities, a discontinuous variation of flutter frequency with Mach number was indicated by the modified strip analysis. An abrupt change of frequency appeared experimentally in the transonic range. (4) Differences in flutter-speed-coefficient levels obtained from tests at low supersonic Mach numbers in two wind tunnels were also predicted by the modified strip analysis and were shown to be caused primarily by differences in mass ratio. (5) Flutter speeds calculated by the subsonic-kernel-function method were in good agreement with experiment and with the results of the modified strip analysis. (6) Flutter speed obtained from piston theory and from quasi-steady second-order theory were higher than experimental values by at least 38 percent.
Book Synopsis AGARD Standard Aeroelastic Configurations for Dynamic Response, I-Wing 445.6 by : A. J. A. Mom
Download or read book AGARD Standard Aeroelastic Configurations for Dynamic Response, I-Wing 445.6 written by A. J. A. Mom and published by . This book was released on 1988 with total page 394 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Journal of Aircraft written by and published by . This book was released on 1972 with total page 528 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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