Deflection And Stress Analysis Of Thin Solid Wings Of Arbitrary Plan Form With Particular Reference To Delta Wings

Author : Manuel Stein,J. Edward Anderson,John M. Hedgepeth
Publisher : Unknown
Page : 60 pages
File Size : 47,6 Mb
Release : 1952
Category : Aeronautics
ISBN : UOM:39015086495754

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Deflection and Stress Analysis of Thin Solid Wings of Arbitrary Plan Form with Particular Reference to Delta Wings by Manuel Stein,J. Edward Anderson,John M. Hedgepeth Pdf

The structural analysis of arbitrary solid cantilever wings by thin-plate theory is reduced to the solution of linear ordinary differential equations by use of the assumption that the chordwise deflections may be expressed in the form of a power series. With the series limited to the first two and the first three terms, the differential equations are solved exactly for several samples of solid delta wings. For cases for which exact solutions to the differential equations cannot be obtained, a numerical procedure is derived. Some experimental data are presented and are found to compare favorably with the present theory.

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 580 pages
File Size : 51,5 Mb
Release : 1956
Category : Aeronautics
ISBN : OSU:32435026188078

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Technical Note - 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 : 1200 pages
File Size : 50,5 Mb
Release : 1954
Category : Aeronautics
ISBN : UOM:39015036314527

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Annual Report of the 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 : 1208 pages
File Size : 51,8 Mb
Release : 1952
Category : Aeronautics
ISBN : CORNELL:31924089884518

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

Author : Almer D. Crim,Donald R. Bellman,Franklin A. Diedrich,Franklin K. Moore,Henry A. Pearson,I. Irving Pinkel,Kenneth A. Foss,Manuel Stein,Ralph W. Stone,United States. National Advisory Committee for Aeronautics,Franklin W. Diedrich,G. Merritt Preston,J. Edward Anderson,Jack C. Humphrey,John P. Reeder,Gerard J. Pesman,James B. Whitten,John M. Hedgepath,Theodore Male
Publisher : Unknown
Page : 344 pages
File Size : 52,9 Mb
Release : 1952
Category : Aerodynamics, Supersonic
ISBN : OSU:32435025004771

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Charts and Approximate Formulas for the Estimation of Aeroelastic Effects on the Lateral Control of Swept and Unswept Wings by Almer D. Crim,Donald R. Bellman,Franklin A. Diedrich,Franklin K. Moore,Henry A. Pearson,I. Irving Pinkel,Kenneth A. Foss,Manuel Stein,Ralph W. Stone,United States. National Advisory Committee for Aeronautics,Franklin W. Diedrich,G. Merritt Preston,J. Edward Anderson,Jack C. Humphrey,John P. Reeder,Gerard J. Pesman,James B. Whitten,John M. Hedgepath,Theodore Male Pdf

Author : Anonim
Publisher : Unknown
Page : 750 pages
File Size : 52,7 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 : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 496 pages
File Size : 46,8 Mb
Release : 1954
Category : Aeronautics
ISBN : IND:30000098997541

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Index of NACA Technical Publications by United States. National Advisory Committee for Aeronautics Pdf

Author : Dean R. Chapman,William R. Wimbrow,Robert H. Kester
Publisher : Unknown
Page : 854 pages
File Size : 51,8 Mb
Release : 1952
Category : Aerodynamics, Supersonic
ISBN : STANFORD:36105024831310

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Experimental Investigation Base Pressure on Blunt-trailing-edge Wings at Supersonic Velocities by Dean R. Chapman,William R. Wimbrow,Robert H. Kester Pdf

The pressres acting on the base of blunt-trailing-edge airfoils have been measured at Mach numbers of 1.25, 1.5, 2.0, and 3.1 and at Reynolds numbers from 0.2 to 3.8 million. Data are presented for 29 profiles both with laminar and with turbulent boundary layers approaching the trailing edges of the wings. The base pressure is found to be a function primarily of Mach number and the ratio of the boundary layer thickeness at the trailing edge to the trailing-edge thickness.

Author : Anonim
Publisher : Unknown
Page : 436 pages
File Size : 47,8 Mb
Release : 1952
Category : Aeronautics
ISBN : UIUC:30112008554161

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Technical Note by Anonim Pdf

Author : Y C Fung
Publisher : Courier Dover Publications
Page : 516 pages
File Size : 51,5 Mb
Release : 2008-10-17
Category : Technology & Engineering
ISBN : 9780486469362

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An Introduction to the Theory of Aeroelasticity by Y C Fung Pdf

Geared toward advanced undergraduates and graduate students, this outstanding text surveys aeroelastic problems, their historical background, basic physical concepts, and the principles of analysis.

Author : Anonim
Publisher : Unknown
Page : 626 pages
File Size : 50,8 Mb
Release : 1952
Category : Mechanics, Applied
ISBN : STANFORD:36105013125773

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Applied Mechanics Reviews by Anonim Pdf

Author : Anonim
Publisher : Unknown
Page : 460 pages
File Size : 40,7 Mb
Release : 1998
Category : Plates (Engineering)
ISBN : PSU:000032591033

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Stability Analysis of Plates and Shells by Anonim Pdf

Author : Defense Documentation Center (U.S.)
Publisher : Unknown
Page : 894 pages
File Size : 46,8 Mb
Release : 1960
Category : Industrial arts
ISBN : UOM:39015024208566

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Subject Index to Unclassified ASTIA Documents by Defense Documentation Center (U.S.) Pdf

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 568 pages
File Size : 54,5 Mb
Release : 1951
Category : Aeronautics
ISBN : IND:30000088900174

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Research Abstracts by United States. National Advisory Committee for Aeronautics Pdf

Author : Allen F. Donovan
Publisher : Princeton University Press
Page : 1021 pages
File Size : 49,5 Mb
Release : 2015-12-08
Category : Science
ISBN : 9781400875030

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High Speed Problems of Aircraft and Experimental Methods by Allen F. Donovan Pdf

Volume VIII of the High Speed Aerodynamics and Jet Propulsion series. This volume includes: performance calculation at high speed; stability and control of high speed aircraft; aeroelasticity and flutter; model testing; transonic wind tunnels; supersonic tunnels; hypersonic experimental facilities; low density wind tunnels; shock tube; wind tunnel measurements; instrumented models in free flight; piloted aircraft testing; free flight range methods. Originally published in 1961. 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.