An Investigation Of Sheet Stiffener Panels Subjected To Compression Loads With Particular Reference To Torsionally Weak Stiffeners
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An Investigation of Sheet stiffener Panels Subjected to Compression Loads with Particular Reference to Torsionally Weak Stiffeners
Author | : Louis Gerhardus Dunn |
Publsiher | : Unknown |
Total Pages | : 96 |
Release | : 1940 |
Genre | : Aluminum alloys |
ISBN | : UOM:39015069157462 |
Download An Investigation of Sheet stiffener Panels Subjected to Compression Loads with Particular Reference to Torsionally Weak Stiffeners Book in PDF, Epub and Kindle
Analytical methods are developed that make it possible for the designer to predict with reasonable accuracy the buckling stress and the maximum-wave amplitude of the sheet in stiffened-panel combinations. The scope of the tests was insufficient to formulate general design criteria but the results are presented as a guide for design and an indication of the type of theoretical and experimental work needed.
An Investigation of Sheet stiffener Panels Subjected to Compression Loads with Particular Reference to Torsionally Weak Stiffeners
Author | : Louis G. Dunn |
Publsiher | : Unknown |
Total Pages | : 576 |
Release | : 1940 |
Genre | : Aluminum alloys |
ISBN | : STANFORD:36105024794971 |
Download An Investigation of Sheet stiffener Panels Subjected to Compression Loads with Particular Reference to Torsionally Weak Stiffeners Book in PDF, Epub and Kindle
Analytical methods are developed that make it possible for the designer to predict with reasonable accuracy the buckling stress and the maximum-wave amplitude of the sheet in stiffened-panel combinations. The scope of the tests was insufficient to formulate general design criteria but the results are presented as a guide for design and an indication of the type of theoretical and experimental work needed.
Index of NACA Technical Publications
Author | : United States. National Advisory Committee for Aeronautics |
Publsiher | : Unknown |
Total Pages | : 1370 |
Release | : 1949 |
Genre | : Aeronautics |
ISBN | : UFL:31262082080614 |
Download Index of NACA Technical Publications Book in PDF, Epub and Kindle
A Selected Listing of NASA Scientific and Technical Reports for
Author | : Anonim |
Publsiher | : Unknown |
Total Pages | : 664 |
Release | : 1949 |
Genre | : Aeronautics |
ISBN | : UVA:X004173284 |
Download A Selected Listing of NASA Scientific and Technical Reports for Book in PDF, Epub and Kindle
Index of Aircraft Structures Research Reports
Author | : United States. National Advisory Committee for Aeronautics |
Publsiher | : Unknown |
Total Pages | : 48 |
Release | : 1947 |
Genre | : Airplanes |
ISBN | : STANFORD:36105112028878 |
Download Index of Aircraft Structures Research Reports Book in PDF, Epub and Kindle
Technical Note National Advisory Committee for Aeronautics
Author | : United States. National Advisory Committee for Aeronautics |
Publsiher | : Unknown |
Total Pages | : 1088 |
Release | : 1952 |
Genre | : Aeronautics |
ISBN | : RUTGERS:39030037542570 |
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Experimental Investigation of a 90 Degree Cascade Diffusing Bend with an Area Ratio of 1 45 1 and with Several Inlet Boundary Layers
Author | : Daniel Friedman |
Publsiher | : Unknown |
Total Pages | : 804 |
Release | : 1952 |
Genre | : Aerodynamics |
ISBN | : STANFORD:36105024831146 |
Download Experimental Investigation of a 90 Degree Cascade Diffusing Bend with an Area Ratio of 1 45 1 and with Several Inlet Boundary Layers Book in PDF, Epub and Kindle
An experimental investigation was conducted in order to determine the performance of a 90 degree cascade diffusing bend with an area ratio of 1.45:1 and a 19-inch square inlet with several inlet-boundary-layer shapes and thicknesses. The maximum mean inlet Mach number was 0.41 and the corresponding airfoil Reynolds number was 950,000. The experimental results seem to indicate that, when the duct configuration requires a bend, a certain amount of diffusion can be obtained without an appreciable rise in the total-pressure losses. If length is important, this configuration requires much less space than the usual diffuser-bend combination.
Critical Compressive Stress for Flat Rectangular Plates Supported Along All Edges and Elastically Restrained Against Rotation Among the Unloaded Edges
Author | : Eugene E. Lundquist,Paul Kuhn,S. Katzoff,Samuel Lévy,Theodore Theodorsen,Thomas A. Harris,United States. National Advisory Committee for Aeronautics,Elbridge Z. Stowell,Harold H. Sweberg,I. E. Garrick,John G. Lowry,Patrick T. Chiarito |
Publsiher | : Unknown |
Total Pages | : 210 |
Release | : 1942 |
Genre | : Aerodynamic load |
ISBN | : OSU:32435063878029 |
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