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Flutter Investigation Of Models Having The Planform Of The North American X 15 Airplane Wing Over A Range Of Mach Numbers 056 To 73
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Book Synopsis Flutter Investigation of Models Having the Planform of the North American X-15 Airplane Wing Over a Range of Mach Numbers Form 0.56 to 7.3 by : Frederick W. Gibson
Download or read book Flutter Investigation of Models Having the Planform of the North American X-15 Airplane Wing Over a Range of Mach Numbers Form 0.56 to 7.3 written by Frederick W. Gibson and published by . This book was released on 1961 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flutter Investigation of Models Having the Planform of the North American X-15 Airplane Wing Over a Range of Mach Numbers 0.56 to 7.3 by :
Download or read book Flutter Investigation of Models Having the Planform of the North American X-15 Airplane Wing Over a Range of Mach Numbers 0.56 to 7.3 written by and published by . This book was released on 1961 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Flutter Investigation of Models of the X-15 Airplane Horizontal Tail by : Lou S. Young
Download or read book Transonic Flutter Investigation of Models of the X-15 Airplane Horizontal Tail written by Lou S. Young and published by . This book was released on 1961 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Flutter Investigation of Models of Proposed Horizontal Tails for the X-15 Airplane by : Lou S. Young
Download or read book Transonic Flutter Investigation of Models of Proposed Horizontal Tails for the X-15 Airplane written by Lou S. Young and published by . This book was released on 1961 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Flutter Investigation of Models of the X-15 Airplane Horizontal Tail by :
Download or read book Transonic Flutter Investigation of Models of the X-15 Airplane Horizontal Tail written by and published by . This book was released on 1961 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flutter Studies of Simplified Component Models of a Variable-sweep-wing Airplane at Mach Numbers Up to 3.0 by : Maynard C. Sandford
Download or read book Flutter Studies of Simplified Component Models of a Variable-sweep-wing Airplane at Mach Numbers Up to 3.0 written by Maynard C. Sandford and published by . This book was released on 1966 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flutter Investigation of a True-speed Dynamic Model with Various Tip-tank Configurations by : John L. Sewall
Download or read book Flutter Investigation of a True-speed Dynamic Model with Various Tip-tank Configurations written by John L. Sewall and published by . This book was released on 1960 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Flutter Investigation of Models of Proposed Horizontal Tails for the X-15 Airplane by :
Download or read book Transonic Flutter Investigation of Models of Proposed Horizontal Tails for the X-15 Airplane written by and published by . This book was released on 1961 with total page 44 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 Investigation of the Aerodynamic Characteristics of a 0.067-scale Model of the X-15 Airplane (configuration 3) at Mach Numbers of 2.29, 2.98, and 4.65 by : Arthur E. Franklin
Download or read book Investigation of the Aerodynamic Characteristics of a 0.067-scale Model of the X-15 Airplane (configuration 3) at Mach Numbers of 2.29, 2.98, and 4.65 written by Arthur E. Franklin and published by . This book was released on 1959 with total page 180 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Flutter Investigation of Some Simple Models of a Boost-glide-vehicle Wing at Mach Numbers of 3.0 and 7.3 by :
Download or read book Experimental Flutter Investigation of Some Simple Models of a Boost-glide-vehicle Wing at Mach Numbers of 3.0 and 7.3 written by and published by . This book was released on 1959 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Planform Curvature Effects on Flutter Characteristics of a Wing with 56 Deg Leading-Edge Sweep and Panel Aspect Ratio of 1.14 by : National Aeronaut Administration (Nasa)
Download or read book Planform Curvature Effects on Flutter Characteristics of a Wing with 56 Deg Leading-Edge Sweep and Panel Aspect Ratio of 1.14 written by National Aeronaut Administration (Nasa) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-10 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental and analytical investigation was initiated to determine the effects of planform curvature (curving the leading and trailing edges of a wing in the X-Y plane) on the transonic flutter characteristics of a series of three moderately swept wing models. Experimental flutter results were obtained in the Langley Transonic Dynamics Tunnel for Mach numbers from 0.60-1.00, with air as the test medium. The models were semispan cantilevered wings with a 3 percent biconvex airfoil and a panel aspect ratio of 1.14. The baseline model had straight leading and trailing edges (i.e., no planform curvature). The radii of curvature of the leading edges for these two models were 200 and 80 inches. The radii of curvature of the leading edges of the other two models were determined so that the root and tip chords were identical for all three models. Experimental results showed that flutter-speed index and flutter frequency ratio increased as planform curvature increase (radius of curvature of the leading edge was decreased) over the test range of Mach numbers. Analytical flutter results were calculated with a subsonic flutter-prediction program, and they agreed well with the experimental results. Keller, Donald F. and Sandford, Maynard C. and Pinkerton, Theresa L. Langley Research Center...
Book Synopsis Transonic Flutter Investigation of Models of a Proposed Variable-sweep Wing by :
Download or read book Transonic Flutter Investigation of Models of a Proposed Variable-sweep Wing written by and published by . This book was released on 1962 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Flutter Investigation of a Fighter-airplane Wing Model and Comparison with a Systematic Plan-form Series by : Norman S. Land
Download or read book Transonic Flutter Investigation of a Fighter-airplane Wing Model and Comparison with a Systematic Plan-form Series written by Norman S. Land and published by . This book was released on 1955 with total page 21 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flight Investigation of Flutter Models with 1/10-scale Douglas D-558-2 Wing Panels by : Jerome M. Teitelbaum
Download or read book Flight Investigation of Flutter Models with 1/10-scale Douglas D-558-2 Wing Panels written by Jerome M. Teitelbaum and published by . This book was released on 1949 with total page 15 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of Wing-aileron Flutter Characteristics of a 1/4-scale Dynamic Model of the X-1E Airplane by : Frederick W. Gibson
Download or read book Experimental Investigation of Wing-aileron Flutter Characteristics of a 1/4-scale Dynamic Model of the X-1E Airplane written by Frederick W. Gibson and published by . This book was released on 1957 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tests to determine some of the flutter characteristics of a 1/4-scale dynamic model of the X-1E airplane wing and aileron were made in the Langley 16-foot transonic tunnel. The wing was tested as part of a complete model of the airplane over a Mach number range of 0.4 to 1.05. Fuselage angles of attack were varied from -14 degrees to 15 degrees at low Mach numbers and from -5 to 4 degrees at higher Mach numbers. Static loading and vibration tests were also performed in still air.
Book Synopsis Planform Curvature Effects on Flutter Characteristics of a Wing with 56 Deg Leading-edge Sweep and Panel Aspect Ratio of 1.14 by :
Download or read book Planform Curvature Effects on Flutter Characteristics of a Wing with 56 Deg Leading-edge Sweep and Panel Aspect Ratio of 1.14 written by and published by . This book was released on 1991 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
