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Supersonic Flutter Of A 60 Degree Delta Wing Encountered During The Flight Test Of A Rocket Propelled Model
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Book Synopsis Supersonic Flutter of a 60 Degrees Delta Wing Encountered During the Flight Test of a Rocket-propelled Model by : Jr. William T. Lauten
Download or read book Supersonic Flutter of a 60 Degrees Delta Wing Encountered During the Flight Test of a Rocket-propelled Model written by Jr. William T. Lauten and published by . This book was released on 1955 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Supersonic Flutter of a 60 Degree Delta Wing Encountered During the Flight Test of a Rocket-propelled Model by : William T. Jr Lauten
Download or read book Supersonic Flutter of a 60 Degree Delta Wing Encountered During the Flight Test of a Rocket-propelled Model written by William T. Jr Lauten and published by . This book was released on 1954 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flutter of a 60 Degree Delta Wing (NACA 65A003 Airfoil) Encountered at Supersonic Speeds During the Flight Test of a Rocket-propelled Model by : Joseph H. Judd
Download or read book Flutter of a 60 Degree Delta Wing (NACA 65A003 Airfoil) Encountered at Supersonic Speeds During the Flight Test of a Rocket-propelled Model written by Joseph H. Judd and published by . This book was released on 1952 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Note on Flutter of a 60 Degree Delta Wing Encountered at Low-supersonic Speeds During the Flight of a Rocket-propelled Model by : William T. Lauten
Download or read book Note on Flutter of a 60 Degree Delta Wing Encountered at Low-supersonic Speeds During the Flight of a Rocket-propelled Model written by William T. Lauten and published by . This book was released on 1951 with total page 21 pages. Available in PDF, EPUB and Kindle. Book excerpt: An analysis of the flight time history of a rocket-propelled model of a 60 degrees delta-wing airplane configuration, fired for the purpose of obtaining zero-lift drag data, indicated wing flutter and subsequent failure at low-supersonic Mach numbers. This flutter occurred during the unpowered decelerating portion of the flight. The behavior of the model during flight is discussed and the mass and stiffness characteristics of a duplicate wing are presented.
Book Synopsis Research Abstracts and Reclassification Notice by : United States. National Advisory Committee for Aeronautics
Download or read book Research Abstracts and Reclassification Notice written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1957 with total page 382 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of Methods for Computing Flutter Characteristics of Supersonic Delta Wings and Comparison with Experimental Data by : Charles Harold Wilts
Download or read book Investigation of Methods for Computing Flutter Characteristics of Supersonic Delta Wings and Comparison with Experimental Data written by Charles Harold Wilts and published by . This book was released on 1959 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Determination of the Effects of Frequency and Amplitude of Oscillation on the Roll-stability Derivatives for a 60 Degree Delta-wing Airplane Model by : Lewis R. Fisher
Download or read book Experimental Determination of the Effects of Frequency and Amplitude of Oscillation on the Roll-stability Derivatives for a 60 Degree Delta-wing Airplane Model written by Lewis R. Fisher and published by . This book was released on 1960 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A New Dimension, Wallops Island Flight Test Range by : Joseph Adams Shortal
Download or read book A New Dimension, Wallops Island Flight Test Range written by Joseph Adams Shortal and published by . This book was released on 1978 with total page 796 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Technical Publications Announcements with Indexes by : United States. National Aeronautics and Space Administration
Download or read book Technical Publications Announcements with Indexes written by United States. National Aeronautics and Space Administration and published by . This book was released on 1962 with total page 1318 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of Low-subsonic Flight Characteristics of a Model of a Hypersonic Boost-glide Configuration Having a 78 Degree Delta Wing /by by : John W. Paulson
Download or read book Investigation of Low-subsonic Flight Characteristics of a Model of a Hypersonic Boost-glide Configuration Having a 78 Degree Delta Wing /by written by John W. Paulson and published by . This book was released on 1961 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis On the Hypersonic Flow Over a Delta Wing with Very Supersonic Leading Edges by : Norman D. Malmuth
Download or read book On the Hypersonic Flow Over a Delta Wing with Very Supersonic Leading Edges written by Norman D. Malmuth and published by . This book was released on 1965 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt: For the case of very supersonic leading edges, the inviscid hypersonic flow over the windward side of a symmetrical flat-plate delta wing at incidence is analyzed. The limit selected is that the incidence is of higher order than the aspect ratio as the incidence tends to zero at infinite Mach number. In this framework, the flow regions consist of a two-dimensional domain adjacent to the leading edges and a central conefield. The flow quantities in the central region represent small linear, rotational perturbations about the zero sweep flow. A Riemann-Poincare boundary value problem for the pressure perturbation is formulated. An additional condition involving the sidewash at the shock is found to be required to resolve the indeterminacy of the foregoing boundary value problem. Series solutions and numerical results are presented for the shock shape and the pressure. The behavior of the latter quantity is found to be similar to that given by the irrotational linear solution for the supersonic leading edge case. Finally, the relationship between the present application and others involving diffraction problems and corner flows is indicated.
Book Synopsis Flight Test and Analysis of the Rolling Motions of a 79 ̊clipped Delta Configuration with Wing-tip Fins at Supersonic Speeds by : James L. Raper
Download or read book Flight Test and Analysis of the Rolling Motions of a 79 ̊clipped Delta Configuration with Wing-tip Fins at Supersonic Speeds written by James L. Raper and published by . This book was released on 1963 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flight Determination of the Drag and Longitudinal Stability and Control Characteristics of a Rocket-powered Model of a 60 Degrees Delta-wing Airplane from Mach Numbers of 0.75 to 1.70 by : Grady L. Mitcham
Download or read book Flight Determination of the Drag and Longitudinal Stability and Control Characteristics of a Rocket-powered Model of a 60 Degrees Delta-wing Airplane from Mach Numbers of 0.75 to 1.70 written by Grady L. Mitcham and published by . This book was released on 1951 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Development, Analysis, and Testing of Cantilevered 6%-thick 70 Degrees Delta Wing Flutter Models, Part I. Supersonic Tests by : Bernard Mazelsky
Download or read book Development, Analysis, and Testing of Cantilevered 6%-thick 70 Degrees Delta Wing Flutter Models, Part I. Supersonic Tests written by Bernard Mazelsky and published by . This book was released on 1963 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Theoretical Investigation of the Subsonic and Supersonic Flutter Characteristics of a Swept Wing Employing a Tuned Sting-mass Flutter Suppressor by : E. Carson Yates
Download or read book Theoretical Investigation of the Subsonic and Supersonic Flutter Characteristics of a Swept Wing Employing a Tuned Sting-mass Flutter Suppressor written by E. Carson Yates and published by . This book was released on 1960 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:
