Use Of Source Distributions For Evaluating Theoretical Aerodynamics Of Thin Finite Wings At Supersonic Speeds

Author : A. J. Eggers,Arthur W. Goldstein,Chung-Hua Wu,Dean R. Chapman,George J. Heimerl,Harvard Lomax,John C. Evvard,John D. Stanitz,Max. A. Heaslet,S. S. Manson,United States. National Advisory Committee for Aeronautics,Artur Mager,Gaylord O. Ellis,Lincoln Wolfestein,Loma Sluder,William M. Roberts,John R. Spreiter
Publisher : Unknown
Page : 264 pages
File Size : 55,5 Mb
Release : 1950
Category : Aerofoils
ISBN : OSU:32435063878391

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Use of Source Distributions for Evaluating Theoretical Aerodynamics of Thin Finite Wings at Supersonic Speeds by A. J. Eggers,Arthur W. Goldstein,Chung-Hua Wu,Dean R. Chapman,George J. Heimerl,Harvard Lomax,John C. Evvard,John D. Stanitz,Max. A. Heaslet,S. S. Manson,United States. National Advisory Committee for Aeronautics,Artur Mager,Gaylord O. Ellis,Lincoln Wolfestein,Loma Sluder,William M. Roberts,John R. Spreiter Pdf

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 996 pages
File Size : 48,6 Mb
Release : 1950
Category : Aeronautics
ISBN : CORNELL:31924089862860

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Report - National Advisory Committee for Aeronautics by United States. National Advisory Committee for Aeronautics Pdf

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 128 pages
File Size : 50,5 Mb
Release : 1955
Category : Aeronautics
ISBN : STANFORD:36105024166121

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Annual Report - National Advisory Committee for Aeronautics by United States. National Advisory Committee for Aeronautics Pdf

Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 38 pages
File Size : 43,6 Mb
Release : 1955
Category : Aeronautics
ISBN : STANFORD:36105024791696

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Report by United States. National Advisory Committee for Aeronautics Pdf

Author : William Rees Sears
Publisher : Princeton University Press
Page : 778 pages
File Size : 55,7 Mb
Release : 2015-12-08
Category : Science
ISBN : 9781400877553

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General Theory of High Speed Aerodynamics by William Rees Sears Pdf

Volume VI of the High Speed Aerodynamics and Jet Propulsion series. This volume includes: physical and mathematical aspects of high speed flows; small perturbation theory; supersonic and transonic small perturbation theory; higher order approximations; nonlinear subsonic and transonic flow theory; nonlinear supersonic steady-flow theory; characteristic methods; flows with shock waves. Originally published in 1954. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.

Author : Elie Carafoli
Publisher : Elsevier
Page : 608 pages
File Size : 43,9 Mb
Release : 2013-10-22
Category : Technology & Engineering
ISBN : 9781483160276

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Wing Theory in Supersonic Flow by Elie Carafoli Pdf

Division II: Aerodynamics, Volume 7: Wing Theory in Supersonic Flow examines the cases of isolated simple wings, wings with vertical plane tail, cruciform wings, and simple or cruciform wings fitted with a body. This book presents the method for the actual calculation of isolated wings or of more complex system. Organized into 12 chapters, this volume starts with an overview of the basic equations in the mechanics of inviscid fluids. This text then presents a unified theory that is established for angularly shaped wings in supersonic flow. Other chapters consider the method for calculating the characteristics of drag, lift, and moments for various shapes of the trailing edge line. This book discusses as well the wings of ordinary shapes, delta wings, yawed wings, polygonal wings, trapezoid wings, and arrow-head or swept-back wings. The final chapter deals with a delta wing with a central fusiform body. This book is a valuable resource for teachers, students, and specialists engaged in modern aerodynamics.

Author : Anonim
Publisher : Unknown
Page : 750 pages
File Size : 41,8 Mb
Release : 1949
Category : Aeronautics
ISBN : UVA:X004173285

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A Selected Listing of NASA Scientific and Technical Reports for ... by Anonim Pdf

Author : Allen F. Donovan
Publisher : Princeton University Press
Page : 863 pages
File Size : 50,7 Mb
Release : 2015-12-08
Category : Science
ISBN : 9781400879908

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Aerodynamic Components of Aircraft at High Speeds by Allen F. Donovan Pdf

Volume VII of the High Speed Aerodynamics and Jet Propulsion series. It deals with applications to specific components of the complete aircraft. Sections of the volume include: aerodynamics of wings at high speed, aerodynamics of bodies at high speed, interaction problems, propellers at high speed, diffusers and nozzles, and nonsteady wing characteristics. Originally published in 1957. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.

Author : Leroy Devan
Publisher : Unknown
Page : 192 pages
File Size : 49,9 Mb
Release : 1980
Category : Angle of attack (Aerodynamics).
ISBN : UOM:39015104954949

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Aerodynamics of Tactical Weapons to Mach Number 8 and Angle of Attack 180° by Leroy Devan Pdf

Author : Elmer A. Horton,Laurence K. Loftin,Stanley F. Racisz
Publisher : Unknown
Page : 678 pages
File Size : 49,6 Mb
Release : 1950
Category : Airplanes
ISBN : STANFORD:36105024796075

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Analysis of the Effects of Boundary-layer Control on the Power-off Landing Performance Characteristics of a Liaison Type of Airplane by Elmer A. Horton,Laurence K. Loftin,Stanley F. Racisz Pdf

An investigation was made to determine the effects of boundary-layer control on the landing performance characteristics of a liaison type of airplane having a payload of 1500 pounds and a flight duration of 5 hours. The aspect ratio was varied from 5 to 15, the wing span from 30 to 100 feet, and the brake horsepower from 300 to 1200. The use of boundary-layer control caused reduction in total landing distance (25 to 40 percent), ground-run distance, gliding speed, and stalling speed whereas sinking speed was increased only slightly.

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 958 pages
File Size : 51,9 Mb
Release : 1955
Category : Aeronautics
ISBN : RUTGERS:39030037542828

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Technical Note - National Advisory Committee for Aeronautics by United States. National Advisory Committee for Aeronautics Pdf

Author : Johns Hopkins University. Applied Physics Laboratory
Publisher : Unknown
Page : 102 pages
File Size : 49,7 Mb
Release : 1957
Category : Aerodynamics, Supersonic
ISBN : UOM:39015006064995

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Handbook of Supersonic Aerodynamics by Johns Hopkins University. Applied Physics Laboratory Pdf

Author : J. J. Chattot,M. M. Hafez
Publisher : Springer
Page : 620 pages
File Size : 42,9 Mb
Release : 2015-03-31
Category : Science
ISBN : 9789401798259

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Theoretical and Applied Aerodynamics by J. J. Chattot,M. M. Hafez Pdf

This book covers classical and modern aerodynamics, theories and related numerical methods, for senior and first-year graduate engineering students, including: -The classical potential (incompressible) flow theories for low speed aerodynamics of thin airfoils and high and low aspect ratio wings. - The linearized theories for compressible subsonic and supersonic aerodynamics. - The nonlinear transonic small disturbance potential flow theory, including supercritical wing sections, the extended transonic area rule with lift effect, transonic lifting line and swept or oblique wings to minimize wave drag. Unsteady flow is also briefly discussed. Numerical simulations based on relaxation mixed-finite difference methods are presented and explained. - Boundary layer theory for all Mach number regimes and viscous/inviscid interaction procedures used in practical aerodynamics calculations. There are also four chapters covering special topics, including wind turbines and propellers, airplane design, flow analogies and hypersonic (rotational) flows. A unique feature of the book is its ten self-tests and their solutions as well as an appendix on special techniques of functions of complex variables, method of characteristics and conservation laws and shock waves. The book is the culmination of two courses taught every year by the two authors for the last two decades to seniors and first-year graduate students of aerospace engineering at UC Davis.

Author : Cornell University. Graduate School of Aeronautical Engineering,Richard W. Hale
Publisher : Unknown
Page : 174 pages
File Size : 55,8 Mb
Release : 1958
Category : Aerodynamics, Supersonic
ISBN : CORNELL:31924004625673

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Aerodynamic Tip Theory of a Supersonic Propeller by Cornell University. Graduate School of Aeronautical Engineering,Richard W. Hale Pdf

Author : Horace John Grover
Publisher : Unknown
Page : 718 pages
File Size : 40,9 Mb
Release : 1951
Category : Airplanes
ISBN : STANFORD:36105024831054

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Fatigue Strengths of Aircraft Materials by Horace John Grover Pdf

This report presents of axial-load fatigue tests on notched specimens of 24S-T3 and 75S-T6 aluminum alloys and normalized SAE 4130 steel with stress-concentration factors of 2.0 (central-circular hole, symmetrical edge notches, and fillets) and 4.0 (symmetrical edge notches and fillets). Fatigue tests were run at several levels of nominal mean stress. Results are compared with previous data for unnotched specimens.