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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
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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 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 Monthly Catalog of United States Government Publications by : United States. Superintendent of Documents
Download or read book Monthly Catalog of United States Government Publications written by United States. Superintendent of Documents and published by . This book was released on 1963 with total page 792 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:
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 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 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 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 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 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 Prediction of Transonic Flutter for a Supercritical Wing by Modified Strip Analysis and Comparison with Experiment by :
Download or read book Prediction of Transonic Flutter for a Supercritical Wing by Modified Strip Analysis and Comparison with Experiment written by and published by . This book was released on 1981 with total page 36 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 Subsonic Flutter Characteristics of a Variable Sweep Wing and Horizontal Tail Combination by : Walter J. Mykytow
Download or read book Subsonic Flutter Characteristics of a Variable Sweep Wing and Horizontal Tail Combination written by Walter J. Mykytow and published by . This book was released on 1970 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt: The project concerns a subsonic investigation of a new type of flutter phenomenon, not previously critical from a design standpoint, involving elastic modes of the wing, fuselage, and stabilizer combination and also involving aerodynamic interference between the wing and horizontal tail. The effort, consisting of design of a flutter model, vibration and subsonic wind tunnel tests, and flutter analyses, was conducted to determine important controlling flutter parameters, to evaluate the accuracy of analyses for predicting the phenomenon, to establish flutter trends and to define flutter prevention design criteria which could be used in the early design stage to avoid the problem. Some of the important features that were determined are increasing wing sweep can lead to lower flutter speeds; wing bending to fuselage torsion frequency ratios were defined which provide the mechanical coupling essential to produce the phenomenon and minimum flutter speeds as a function of wing sweep angle; vertical separation or dihedral angle can be very influential and beneficial and is more important than longitudinal separation, the effects of which were found to be small to moderate; the effects of compressibility have been shown to be detrimental and decrease the flutter speed, and conclusive proof that the interference aerodynamics between the wind and tail, and particularly, the downwash shed from the wing, is an important and detrimental feature to the phenomenon. (Author).
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 Relationship Between Flutter Parameters and Generalized Aerodynamic Forces for Wings of Low Aspect Ratio by : Bernard Mazelsky
Download or read book Relationship Between Flutter Parameters and Generalized Aerodynamic Forces for Wings of Low Aspect Ratio written by Bernard Mazelsky and published by . This book was released on 1962 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt: A set of closed-form approximations is derived which relates the flutter conditions of a wing to its generalized aerodynamic forces. A simplified two-mode analysis is used to obtain a firstorder approximation. More general analyses are performed by treating additional effects as perturbations. The derivations are applicable to a wide class of low-aspect-ratio wings and apply to subsonic, transonic, supersonic, and hypersonic flow.
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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