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Book An Investigation of Sheet stiffener Panels Subjected to Compression Loads with Particular Reference to Torsionally Weak Stiffeners

Download or read book An Investigation of Sheet stiffener Panels Subjected to Compression Loads with Particular Reference to Torsionally Weak Stiffeners written by Louis G. Dunn and published by . This book was released on 1940 with total page 576 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.

Book An Investigation of Sheet stiffener Panels Subjected to Compression Loads with Particular Reference to Torsionally Weak Stiffeners

Download or read book An Investigation of Sheet stiffener Panels Subjected to Compression Loads with Particular Reference to Torsionally Weak Stiffeners written by Louis Gerhardus Dunn and published by . This book was released on 1940 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.

Book An Investigation of Sheet stiffener Panels Subjected to Compression Loads with Particular Reference to Torsionally Weak Stiffness

Download or read book An Investigation of Sheet stiffener Panels Subjected to Compression Loads with Particular Reference to Torsionally Weak Stiffness written by Louis G. Dunn and published by . This book was released on 1940 with total page 59 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Index of NACA Technical Publications

Download or read book Index of NACA Technical Publications written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1949 with total page 1370 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Selected Listing of NASA Scientific and Technical Reports for

Download or read book A Selected Listing of NASA Scientific and Technical Reports for written by and published by . This book was released on 1949 with total page 664 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Index of Aircraft Structures Research Reports

Download or read book Index of Aircraft Structures Research Reports written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1947 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Technical Note   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 1088 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Experimental Investigation of a 90 Degree Cascade Diffusing Bend with an Area Ratio of 1 45 1 and with Several Inlet Boundary Layers

Download or read book Experimental Investigation of a 90 Degree Cascade Diffusing Bend with an Area Ratio of 1 45 1 and with Several Inlet Boundary Layers written by Daniel Friedman and published by . This book was released on 1952 with total page 804 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.

Book Critical Compressive Stress for Flat Rectangular Plates Supported Along All Edges and Elastically Restrained Against Rotation Among the Unloaded Edges

Download or read book Critical Compressive Stress for Flat Rectangular Plates Supported Along All Edges and Elastically Restrained Against Rotation Among the Unloaded Edges written by Eugene E. Lundquist and published by . This book was released on 1942 with total page 210 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Strength of Aircraft Elements

Download or read book Strength of Aircraft Elements written by and published by . This book was released on 1940 with total page 152 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Strength of Air Craft Elements   with List of References

Download or read book Strength of Air Craft Elements with List of References written by United States. Army-Navy Civil Committee on Aircraft Design Criteria and published by . This book was released on 1942 with total page 162 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Annual Report of the 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 1939 with total page 546 pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes the Committee's Reports no. 1-1058, reprinted in v. 1-37.

Book Report   National Advisory Committee for Aeronautics

Download or read book Report National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1940 with total page 550 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Buckling Experiments  Experimental Methods in Buckling of Thin Walled Structures  Volume 2

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.

Book Catalogue of the Public Documents of the     Congress and of All Departments of the Government of the United States for the Period from     to

Download or read book Catalogue of the Public Documents of the Congress and of All Departments of the Government of the United States for the Period from to written by United States. Superintendent of Documents and published by . This book was released on with total page 2868 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book ANC Bulletin

    Book Details:
  • Author : United States. Munitions Board. Aircraft Committee. Subcommittee on Air Force, Navy, Civil Aircraft Design Criteria
  • Publisher :
  • Release : 1942
  • ISBN :
  • Pages : 162 pages

Download or read book ANC Bulletin written by United States. Munitions Board. Aircraft Committee. Subcommittee on Air Force, Navy, Civil Aircraft Design Criteria and published by . This book was released on 1942 with total page 162 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Bulletin

    Book Details:
  • Author : Texas Engineering Experiment Station
  • Publisher :
  • Release : 1847
  • ISBN :
  • Pages : 136 pages

Download or read book Bulletin written by Texas Engineering Experiment Station and published by . This book was released on 1847 with total page 136 pages. Available in PDF, EPUB and Kindle. Book excerpt: