The Effect of Nonuniform Temperature Distributions on the Stresses and Distortions of Stiffened-shell Structures

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ISBN 13 :
Total Pages : 56 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis The Effect of Nonuniform Temperature Distributions on the Stresses and Distortions of Stiffened-shell Structures by : Richard R. Heldenfels

Download or read book The Effect of Nonuniform Temperature Distributions on the Stresses and Distortions of Stiffened-shell Structures written by Richard R. Heldenfels and published by . This book was released on 1950 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt: The structural effects of nonuniform temperature distributions, such as those produced by aerodynamic heating or thermal ice-prevention systems, are discussed and found to be of two types: The introduction of thermal stresses and distortions as a result of restrained thermal expansion and a change in the stresses and distortions produced by the applied loads as a result of the variation of elastic properties of materials with temperature. These effects are illustrated by sample analyses of the stress and distortion distributions of simple box beams and by calculation of the stresses on a typical wing section.

A Numerical Method for the Stress Analysis of Stiffened-shell Structures Under Nonuniform Temperature Distributions

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Publisher :
ISBN 13 :
Total Pages : 54 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis A Numerical Method for the Stress Analysis of Stiffened-shell Structures Under Nonuniform Temperature Distributions by : Richard R. Heldenfels

Download or read book A Numerical Method for the Stress Analysis of Stiffened-shell Structures Under Nonuniform Temperature Distributions written by Richard R. Heldenfels and published by . This book was released on 1950 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt: A numerical method is presented for the stress analysis of stiffened-shell structures of arbitrary cross section under nonuniform temperature distributions. The method is based on a previously published procedure that is extended to include temperature effects and multicell construction. The applicationof the method to practical problems is discussed and an illustrative analysis is presented of a two-cell box beam under the combined action of vertical loads and nonuniform temperature distribution.

Buckling Experiments: Experimental Methods in Buckling of Thin-Walled Structures, Volume 2

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Publisher : John Wiley & Sons
ISBN 13 : 0471974501
Total Pages : 1140 pages
Book Rating : 4.4/5 (719 download)

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Book Synopsis Buckling Experiments: Experimental Methods in Buckling of Thin-Walled Structures, Volume 2 by : Josef Singer

Download or read book Buckling Experiments: Experimental Methods in Buckling of Thin-Walled Structures, Volume 2 written by Josef Singer and published by John Wiley & Sons. This book was released on 2002-08-12 with total page 1140 pages. Available in PDF, EPUB and Kindle. Book excerpt: * Edited by Josef Singer, the world's foremost authority on structural buckling. * Time-saving and cost-effective design data for all structural, mechanical, and aerospace engineering researchers.

NASA Technical Memorandum

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ISBN 13 :
Total Pages : 92 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis NASA Technical Memorandum by :

Download or read book NASA Technical Memorandum written by and published by . This book was released on 1982 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt:

List of Technical Notes, 1947-1953

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ISBN 13 :
Total Pages : 162 pages
Book Rating : 4.0/5 ( download)

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Book Synopsis List of Technical Notes, 1947-1953 by : United States. National Advisory Committee for Aeronautics

Download or read book List of Technical Notes, 1947-1953 written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1954 with total page 162 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Stress and Distortion Analysis of a Swept Box Beam Having Bulkheads Perpendicular to the Spars

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Publisher :
ISBN 13 :
Total Pages : 712 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Stress and Distortion Analysis of a Swept Box Beam Having Bulkheads Perpendicular to the Spars by : Richard R. Heldenfels

Download or read book Stress and Distortion Analysis of a Swept Box Beam Having Bulkheads Perpendicular to the Spars written by Richard R. Heldenfels and published by . This book was released on 1950 with total page 712 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method is presented for the approximate calculation of the stresses and distortions in a box beam representing the main structural component of a swept wing with a carry-through section and with bulkheads perpendicular to the spars. The application of the method is illustrated by a numerical example and its results are compared with previously published test data.

Experimental and Theoretical Determination of Thermal Stresses in a Flat Plate

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Publisher :
ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Experimental and Theoretical Determination of Thermal Stresses in a Flat Plate by : Richard R. Heldenfels

Download or read book Experimental and Theoretical Determination of Thermal Stresses in a Flat Plate written by Richard R. Heldenfels and published by . This book was released on 1952 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: Thermal stresses induced in a flat, rectangular, 75S-T6 aluminum-alloy plate by nonuniform heating are determined both experimentally and theoretically. The characteristics of commercially available bonded resistance wire strain gages are first investigated to determine their suitability for measuring stresses under simple conditions of stress and temperature. The gages are then used to measure thermal stresses in the flat plate in order to study their suitability under more complicated conditions. The experimental results are found to be in satisfactory agreement (within plus or minus 5 percent of maximum calculated stress) with an approximate theoretical solution of the problem.

Monthly Catalog of United States Government Publications

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Publisher :
ISBN 13 :
Total Pages : 1376 pages
Book Rating : 4.3/5 (121 download)

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Book Synopsis Monthly Catalog of United States Government Publications by :

Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 1951 with total page 1376 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Annual Report of the National Advisory Committee for Aeronautics

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Publisher :
ISBN 13 :
Total Pages : 1464 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Annual Report of the National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics

Download or read book Annual Report of the National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1950 with total page 1464 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Bibliography of Technical Reports

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ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Bibliography of Technical Reports by :

Download or read book Bibliography of Technical Reports written by and published by . This book was released on 1951 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Bibliography on Shells and Shell-like Structures

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Publisher :
ISBN 13 :
Total Pages : 164 pages
Book Rating : 4.X/5 ( download)

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Book Synopsis Bibliography on Shells and Shell-like Structures by : William Arthur Nash

Download or read book Bibliography on Shells and Shell-like Structures written by William Arthur Nash and published by . This book was released on 1954 with total page 164 pages. Available in PDF, EPUB and Kindle. Book excerpt:

WADC Technical Report

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Publisher :
ISBN 13 :
Total Pages : 1286 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis WADC Technical Report by : United States. Wright Air Development Division

Download or read book WADC Technical Report written by United States. Wright Air Development Division and published by . This book was released on 1955 with total page 1286 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Applied Mechanics Reviews

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ISBN 13 :
Total Pages : 934 pages
Book Rating : 4.:/5 (26 download)

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Book Synopsis Applied Mechanics Reviews by :

Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1948 with total page 934 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Numerical Method for the Stress Analysis of Stiffened-shell Structures Under Nonuniform Temperature Distributions

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Publisher :
ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.:/5 (25 download)

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Book Synopsis A Numerical Method for the Stress Analysis of Stiffened-shell Structures Under Nonuniform Temperature Distributions by : Richard R. Heldenfels

Download or read book A Numerical Method for the Stress Analysis of Stiffened-shell Structures Under Nonuniform Temperature Distributions written by Richard R. Heldenfels and published by . This book was released on 1951 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Experimental Investigation of the Effect of Vertical-tail Size and Length and of Fuselage Shape and Length on the Static Lateral Stability Characteristics of a Model with 45 ̊sweptback Wing and Tail Surfaces

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Publisher :
ISBN 13 :
Total Pages : 328 pages
Book Rating : 4.3/5 (243 download)

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Book Synopsis Experimental Investigation of the Effect of Vertical-tail Size and Length and of Fuselage Shape and Length on the Static Lateral Stability Characteristics of a Model with 45 ̊sweptback Wing and Tail Surfaces by : Antonio Ferri

Download or read book Experimental Investigation of the Effect of Vertical-tail Size and Length and of Fuselage Shape and Length on the Static Lateral Stability Characteristics of a Model with 45 ̊sweptback Wing and Tail Surfaces written by Antonio Ferri and published by . This book was released on 1951 with total page 328 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Wear and Sliding Friction Properties of Nickel Alloys Suited for Cages of High-temperature Rolling-contact Bearings

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ISBN 13 :
Total Pages : 754 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Wear and Sliding Friction Properties of Nickel Alloys Suited for Cages of High-temperature Rolling-contact Bearings by : Robert L. Johnson

Download or read book Wear and Sliding Friction Properties of Nickel Alloys Suited for Cages of High-temperature Rolling-contact Bearings written by Robert L. Johnson and published by . This book was released on 1952 with total page 754 pages. Available in PDF, EPUB and Kindle. Book excerpt: Wear and sliding friction properties of a number of nickel alloys operating against hardened SAE 52100 steel were studied. The alloys were cast beryllium nickel, heat-treated beryllium nickel, cast Inconel, Nimonic 80, Inconel X, Refractalloy 26, and Discaloy. Some of the allows studied may be useful as material for cages of rolling-contact bearings that operate at high speeds with temperatures above 600 degrees F in projected aircraft turbine engines or for bearings that operate in corrosive mediums. Desirable operating properties and the absence of extreme mass welding of all the materials could be associated with the development of the sliding surfaces of a naturally formed film of nickel oxide. On the basis of wear and friction properties, cast Inconel performed very well in these experiments and compares favorably with nodular iron. Nimonic 80 also showed promise as a possible cage material.

Technical Note - National Advisory Committee for Aeronautics

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Publisher :
ISBN 13 :
Total Pages : 802 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis Technical Note - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics

Download or read book Technical Note - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1952 with total page 802 pages. Available in PDF, EPUB and Kindle. Book excerpt: