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Investigation Of The Subsonic Flutter Characteristics Of A Highly Swept Arrow Planform Wing With And Without Simulated Trailing Edge Mounted Engine Masses
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Book Synopsis Investigation of the Subsonic Flutter Characteristics of a Highly Swept Arrow Planform Wing with and Without Simulated Trailing-edge-mounted Engine Masses by : Gerald David Walberg
Download or read book Investigation of the Subsonic Flutter Characteristics of a Highly Swept Arrow Planform Wing with and Without Simulated Trailing-edge-mounted Engine Masses written by Gerald David Walberg and published by . This book was released on 1962 with total page 168 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Flutter Tests of a Highly Swept Arrow Wing with and Without Simulated Trailing-edge-mounted Engine Masses by : Gerald D. Walberg
Download or read book Transonic Flutter Tests of a Highly Swept Arrow Wing with and Without Simulated Trailing-edge-mounted Engine Masses written by Gerald D. Walberg and published by . This book was released on 1962 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Proceedings of NASA Conference on Supersonic-Transport Feasibility Studies and Supporting Research, September 17-19, 1963, Langley Research Center, Langley Station, Hampton, Va by :
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:
Book Synopsis Transonic Flutter Tests of a Highly Swept Arrow Wing with and Without Simulated Trailing-edge-mounted Engine Masses by : Gerald D. Walberg
Download or read book Transonic Flutter Tests of a Highly Swept Arrow Wing with and Without Simulated Trailing-edge-mounted Engine Masses written by Gerald D. Walberg and published by . This book was released on 1962 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: Transonic flutter tests were made for three series of cantilevered semispan wing models which had arrow planforms and leading-edge sweep angles of 72.5 degrees. The first series were basic wing panels; the second series carried simulated engine masses and nacelles located at 34.9, 55.8, and 76.6% of the semispan; the third series carried only lightweight nacelles. The mass of each simulated engine was approximately 41% of the basic wing-panel mass. At Mach numbers below 0.975, the addition of the engine masses increased the flutter dynamic pressure of the basic wings; the nacelles do not affect the flutter boundary of the basic wings in this Mach number range. At Mach numbers above 1.05 the flutter boundary for the wings with engine masses and nacelles was higher than the boundary of the basic wings, but below the boundary for the wings with only lightweight nacelles. (Author).
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 1961 with total page 1248 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Monthly Catalog of United States Government Publications, Cumulative Index by : United States. Superintendent of Documents
Download or read book Monthly Catalog of United States Government Publications, Cumulative Index written by United States. Superintendent of Documents and published by . This book was released on 1979 with total page 1250 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Proceedings of NASA Conference on Supersonic-transport Feasibility Studies and Supporting Research by :
Download or read book Proceedings of NASA Conference on Supersonic-transport Feasibility Studies and Supporting Research written by and published by . This book was released on 1963 with total page 526 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 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 International Aerospace Abstracts by :
Download or read book International Aerospace Abstracts written by and published by . This book was released on 1992 with total page 1210 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Masters Theses in the Pure and Applied Sciences Accepted by Colleges and Universities of the United States by :
Download or read book Masters Theses in the Pure and Applied Sciences Accepted by Colleges and Universities of the United States written by and published by . This book was released on 1966 with total page 446 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 An Investigation of the Flutter Characteristics of Swept Wings at Subsonic Speeds by : H. W. Hannah
Download or read book An Investigation of the Flutter Characteristics of Swept Wings at Subsonic Speeds written by H. W. Hannah and published by . This book was released on 1948 with total page 143 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low-speed Aerodynamic Characteristics of a Highly Swept, Untwisted, Uncambered Arrow Wing by : Paul L. Coe
Download or read book Low-speed Aerodynamic Characteristics of a Highly Swept, Untwisted, Uncambered Arrow Wing written by Paul L. Coe and published by . This book was released on 1983 with total page 76 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 1971 with total page 1330 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Parametric Flutter Studies of an Arrow-wing Configuration: Some Early Results by :
Download or read book Parametric Flutter Studies of an Arrow-wing Configuration: Some Early Results written by and published by . This book was released on 1988 with total page 24 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:
