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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
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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:
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 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 Use of Experimental Steady-flow Aerodynamic Parameters in Calculation of Flutter Characteristics for Finite-span Swept Or Unswept Wings at Subsonic, Transonic Speeds [with List of References] by :
Download or read book Use of Experimental Steady-flow Aerodynamic Parameters in Calculation of Flutter Characteristics for Finite-span Swept Or Unswept Wings at Subsonic, Transonic Speeds [with List of References] written by and published by . This book was released on 1960 with total page 51 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 Calculation of Flutter Characteristics for Finite-span Swept Or Unswept Wings at Subsonic and Supersonic Speeds by a Modified Strip Analysis by : E. Carson Jr Yates
Download or read book Calculation of Flutter Characteristics for Finite-span Swept Or Unswept Wings at Subsonic and Supersonic Speeds by a Modified Strip Analysis written by E. Carson Jr Yates and published by . This book was released on 1958 with total page 121 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flutter Characteristics of Swept Wings at Transonic Speeds by : Laurence K. Loftin
Download or read book Flutter Characteristics of Swept Wings at Transonic Speeds written by Laurence K. Loftin and published by . This book was released on 1955 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Calculation of Flutter Characteristics for Finite-span Swept Or Unswept Wings at Subsonic, Transonic, and Supersonic Speeds by a Modified Strip Analysis by : Edward Carson Yates
Download or read book Calculation of Flutter Characteristics for Finite-span Swept Or Unswept Wings at Subsonic, Transonic, and Supersonic Speeds by a Modified Strip Analysis written by Edward Carson Yates and published by . This book was released on 1959 with total page 494 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Subsonic Aerodynamic and Flutter Characteristics of Several Wings Calculated by the SOUSSA P1.1 Panel Method by : Edward Carson Yates
Download or read book Subsonic Aerodynamic and Flutter Characteristics of Several Wings Calculated by the SOUSSA P1.1 Panel Method written by Edward Carson Yates and published by . This book was released on 1982 with total page 24 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 Comparisons of Some Wing Flutter Characteristics Obtained by Modified Strip Analysis, Subsonic Kernel Function, and Experiment by : Edward Carson Yates
Download or read book Comparisons of Some Wing Flutter Characteristics Obtained by Modified Strip Analysis, Subsonic Kernel Function, and Experiment written by Edward Carson Yates and published by . This book was released on 1964 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Some Effects of Tip Fins of Wing Flutter Characteristics by : Robert Charles Goetz
Download or read book Some Effects of Tip Fins of Wing Flutter Characteristics written by Robert Charles Goetz and published by . This book was released on 1974 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Lift, Pitching Moment, and Span Load Characteristics of Wings at Low Speed as Affected by Variations of Sweep and Aspect Ratio by : Edward J. Hopkins
Download or read book Lift, Pitching Moment, and Span Load Characteristics of Wings at Low Speed as Affected by Variations of Sweep and Aspect Ratio written by Edward J. Hopkins and published by . This book was released on 1951 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lift, pitching-moment, and pressure distribution were measured on a wing which was swept -40, -30, 0, 35, and 45 degrees. The wing span was decreased to give aspect ratios 6.8, 5.3, 4.2, 3.4, and 2.8. The effects of independent variations of sweep and aspect ratio on the lift, pitching-moment, and span-load characteristics of the wings are compared with the effects estimated by use of the Weissinger method.
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 Investigation of Transonic Flutter Characteristics of a Thin 10 Degree Sweptback Wing Having an Aspect Ratio of 4 and a Taper Ratio of 0.6 by : George W. Jones
Download or read book Investigation of Transonic Flutter Characteristics of a Thin 10 Degree Sweptback Wing Having an Aspect Ratio of 4 and a Taper Ratio of 0.6 written by George W. Jones and published by . This book was released on 1957 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: A flutter investigation has been made in the Langley transonic blowdown tunnel at Mach numbers between 0.79 and 1.34 on a thin 10 degree sweptback wing having an aspect ratio of 4 and a taper ratio of 0.6. The data obtained have been compared with data from NACA Research Memorandum L55I13A for zero and 30 degree sweptback wings of the type investigated, the flutter boundary for the 10 degree sweptback wing falls between those for the zero degree and 30 degree sweptback wings in the low supersonic Mach number range. However, the subsonic level (around a Mach number of 0.8) of the flutter boundary for the 10 degree sweptback wing lies above those for the zero and 30 degree sweptback wings. In addition, the amount of rise in the flutter boundary from the subsonic level to the supersonic values is about the same for the wings with angles of sweepback of 10 degrees and zero degrees, but is much greater for the wing with an angle of sweepback of 30 degrees.
Book Synopsis Preliminary Study of Some Factors which Affect the Stall-flutter Characteristics of Thin Wings by : A. Gerald Rainey
Download or read book Preliminary Study of Some Factors which Affect the Stall-flutter Characteristics of Thin Wings written by A. Gerald Rainey and published by . This book was released on 1952 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: Some of the other factors considered were found to be more or less significant however, all the factors will require further study if their effects are to be more fully interpreted.
Book Synopsis A Plan-form Parameter for Correlating Certain Aerodynamic Characteristics of Swept Wings by : Franklin W. Diederich
Download or read book A Plan-form Parameter for Correlating Certain Aerodynamic Characteristics of Swept Wings written by Franklin W. Diederich and published by . This book was released on 1951 with total page 17 pages. Available in PDF, EPUB and Kindle. Book excerpt: The finite-span effects on the lift-curve slope and the coefficient of damping in roll of swept wings in subsonic flow are shown to be functions primarily of a parameter which incorporates the aspect ratio, the sweep, and the section lift-curve slope. The limitations and possible uses of this parameter are discussed.
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