Comparison Between Theoretical And Experimental Stresses In Circular Semimonocoque Cylinders With Rectangular Cutouts

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Comparison Between Theoretical and Experimental Stresses in Circular Semimonocoque Cylinders with Rectangular Cutouts

Author : Harvey G. McComb,Emmet F. Low
Publisher : Unknown
Page : 702 pages
File Size : 54,7 Mb
Release : 1955
Category : Cylinders
ISBN : STANFORD:36105024832037

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Comparison Between Theoretical and Experimental Stresses in Circular Semimonocoque Cylinders with Rectangular Cutouts by Harvey G. McComb,Emmet F. Low Pdf

Comparisons are made between a theory for calculating stresses about rectangular cutouts in circular cylinders of semimonocoque construction published in NACA TN 3200 and previously published NACA experimental data. The comparisons include stresses in the stringers and shear stresses in the center of the shear panels in the neighborhood of the cutout. The theory takes into account the bending flexibility of the rings in the structure, and this factor is found to be important in the calculation of stresses about cutouts. In general, when the ring flexibility is considered, good agreement is exhibited between the calculated and experimental results.

Technical Note - National Advisory Committee for Aeronautics

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 790 pages
File Size : 42,6 Mb
Release : 1955
Category : Aeronautics
ISBN : RUTGERS:39030037545607

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

Applied Mechanics Reviews

Author : Anonim
Publisher : Unknown
Page : 616 pages
File Size : 54,8 Mb
Release : 1948
Category : Mechanics, Applied
ISBN : UCAL:C2682411

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Applied Mechanics Reviews by Anonim Pdf

Research Abstracts

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 568 pages
File Size : 45,6 Mb
Release : 1951
Category : Aeronautics
ISBN : IND:30000088900174

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

Research Abstracts and Reclassification Notice

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 508 pages
File Size : 41,7 Mb
Release : 1954
Category : Aeronautics
ISBN : IND:30000098603164

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

NASA Technical Translation

Author : Anonim
Publisher : Unknown
Page : 1026 pages
File Size : 44,5 Mb
Release : 1970
Category : Aeronautics
ISBN : UOM:39015047365666

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NASA Technical Translation by Anonim Pdf

Aero Digest

Author : Anonim
Publisher : Unknown
Page : 1130 pages
File Size : 46,7 Mb
Release : 1955
Category : Aeronautics
ISBN : STANFORD:36105117568902

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Aero Digest by Anonim Pdf

Annual Report - National Advisory Committee for Aeronautics

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 128 pages
File Size : 49,8 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.

Report

Author : Anonim
Publisher : Unknown
Page : 522 pages
File Size : 40,6 Mb
Release : 1953
Category : Aeronautics
ISBN : UIUC:30112108397438

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Report by Anonim Pdf

U.S. Government Research Reports

Author : Anonim
Publisher : Unknown
Page : 74 pages
File Size : 41,9 Mb
Release : 1957
Category : Science
ISBN : UOM:39015086571323

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U.S. Government Research Reports by Anonim Pdf

Index of NACA Technical Publications

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 580 pages
File Size : 42,6 Mb
Release : 1956
Category : Aeronautics
ISBN : UCBK:C029901318

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

A Theoretical Investigation of the Aerodynamics of Wing-tail Combinations Performing Time-dependent Motions at Supersonic Speeds

Author : John C. Martin,Margaret S. Diederich,Percy J. Bobbitt
Publisher : Unknown
Page : 720 pages
File Size : 47,8 Mb
Release : 1954
Category : Aerodynamics, Supersonic
ISBN : STANFORD:36105024831682

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A Theoretical Investigation of the Aerodynamics of Wing-tail Combinations Performing Time-dependent Motions at Supersonic Speeds by John C. Martin,Margaret S. Diederich,Percy J. Bobbitt Pdf

A theoretical investigation is presented of the contribution of horizontal tails to the lift and pitching moment due to angle of attack, a constant rate of pitch, and a constant vertical acceleration. Numerical values of the aerodynamic coefficients associated with these motions are presented for a number of two-dimensional wing-tail combinations, a triangular wing-tail combination, and a number of rectangular-wing - triangular-tail combinations.