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Book Bearing Strengths of Some Wrought aluminum Alloys

Download or read book Bearing Strengths of Some Wrought aluminum Alloys written by R. L. Moore and published by . This book was released on 1943 with total page 584 pages. Available in PDF, EPUB and Kindle. Book excerpt: Although a number of investigations of the bearing strength of aluminum alloys have been made, the problem remains one of considerable interest to the aircraft industry. For this reason it has seemed advisable to make additional tests of the commonly used aircraft alloys in an effort to establish a better basis for the selection of allowable bearing values. Current design practice does not recognize the effect of edge distance upon bearing strengths, and for this reason edge distance upon bearing strengths, and for this reason edge distance was one of the principal variables considered in this investigation. The increasing emphasis being placed upon permanent set limitations makes it essential that more information on bearing yield phenomena be obtained.

Book Bearing Strengths of Some Wrought aluminium Alloys

Download or read book Bearing Strengths of Some Wrought aluminium Alloys written by R.L. Moore and published by . This book was released on 1943 with total page 19 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Bearing Strengths of 75S T Aluminum alloy Sheet and Extruded Angle

Download or read book Bearing Strengths of 75S T Aluminum alloy Sheet and Extruded Angle written by C. Wescoat and published by . This book was released on 1945 with total page 6 pages. Available in PDF, EPUB and Kindle. Book excerpt: Several reports have been issued covering the bearing properties of the wrought aluminum alloys commonly used in aircraft constructioin. The development of the new high-strength all0y 75S-T has made bearing tests of this material desirable.

Book Bearing Strengths of Some Aluminum alloy Permanent mold Castings

Download or read book Bearing Strengths of Some Aluminum alloy Permanent mold Castings written by E. M. Finley and published by . This book was released on 1951 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results are presented in this paper of bearing tests made to determine bearing ultimate and yield strengths of aluminum-alloy permanent-mold castings of B195-T4, B195-T6, and 356-T6, and to compare the ratios of bearing to tensile properties obtained with similar data from sand-castings of like materials.

Book Bearing Strengths of Bare and Alclad XA75S T and 25S T81 Aluminum Alloy Sheet

Download or read book Bearing Strengths of Bare and Alclad XA75S T and 25S T81 Aluminum Alloy Sheet written by R. L. Moore and published by . This book was released on 1943 with total page 6 pages. Available in PDF, EPUB and Kindle. Book excerpt: A report was recently issued covering an investigation of the bearing properties of the wrought aluminum alloys commonly used in aircraft construction. Since this work was undertaken, two new materials, XA75S-T and 24S-T81,have been developed to the commercial stage for aircraft use. THe object of this investigation was to determine the bearing yield and ultimate strengths of these new materials in the form of bare and alclad sheet.

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 1951 with total page 936 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Technical Note

Download or read book Technical Note written by and published by . This book was released on with total page 490 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Method for Estimating Heat Requirements for Ice Prevention on Gas heated Hollow Propeller Blades

Download or read book A Method for Estimating Heat Requirements for Ice Prevention on Gas heated Hollow Propeller Blades written by V. H. Gray and published by . This book was released on 1947 with total page 602 pages. Available in PDF, EPUB and Kindle. Book excerpt: A detailed method is presented for determining temperature and flow minimums of heated gas necessary for ice prevention of hollow propellers with evaluation of surface temperatures, gas pressures, tip nozzle areas, flow passages, and heat source input.

Book Some Investigations of the General Instability of Stiffened Metal Cylinders

Download or read book Some Investigations of the General Instability of Stiffened Metal Cylinders written by Daniel Guggenheim Aeronautical Laboratory and published by . This book was released on 1943 with total page 656 pages. Available in PDF, EPUB and Kindle. Book excerpt: This is the sixth of a series of report covering an investigation of the general instability problem by the California Institute of Technology. This report summarizes the work that has been carried on in the experimental investigation of the problem of general instability of stiffened metal cylinders subjected to combined bending and transverse shear.

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 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 616 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Strength of Metal Aircraft Elements

Download or read book Strength of Metal Aircraft Elements written by United States. Department of Defense and published by . This book was released on 1961 with total page 382 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Strength of Metal Aircraft Elements

Download or read book Strength of Metal Aircraft Elements written by United States. ANC-5 Panel on Strength of Metal Aircraft Elements and published by . This book was released on 1955 with total page 200 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Strength of Metal Aircraft Elements

    Book Details:
  • Author : United States. Munitions Board. Aircraft Committee. Subcommittee on Air Force-Navy-Civil Aircraft Design Criteria
  • Publisher :
  • Release : 1955
  • ISBN :
  • Pages : 202 pages

Download or read book Strength of Metal Aircraft Elements 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 1955 with total page 202 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Effect of Aging Aircraft Structures on Magnesium Parts

Download or read book Effect of Aging Aircraft Structures on Magnesium Parts written by A. W. Winston and published by . This book was released on 1945 with total page 716 pages. Available in PDF, EPUB and Kindle. Book excerpt: The forms in which magnesium alloys may be encountered are castings, extrusions, forgings, and sheet. The alloys commonly used in aircraft structures in the various forms and the effects of the aging treatment are discussed under separate headings below.

Book Applied Mechanics Reviews

Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1948 with total page 446 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Effect of Small Deviations from Flatness on Effective Width and Buckling of Plates in Compression

Download or read book Effect of Small Deviations from Flatness on Effective Width and Buckling of Plates in Compression written by Pai C. Hu and published by . This book was released on 1946 with total page 544 pages. Available in PDF, EPUB and Kindle. Book excerpt: (3) The Southwell plot method of predicting theoretical critical stresses for perfect specimens from experimental observations on actual specimens may not be expected to give, in general, satisfactory results when applied to flat plates.