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Experimental Investigation Of Cylinders Subjected To Pure Bending
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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 1957 with total page 836 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Note written by and published by . This book was released on 1964 with total page 542 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
Book Synopsis Index of NACA Technical Publications by : United States. National Advisory Committee for Aeronautics
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 1952 with total page 498 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 1946 with total page 648 pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Book Synopsis Notes and Tables for Use in the Analysis of Supersonic Flow by :
Download or read book Notes and Tables for Use in the Analysis of Supersonic Flow written by and published by . This book was released on 1947 with total page 594 pages. Available in PDF, EPUB and Kindle. Book excerpt: This document is a compilation of formulas, tables, and curves for use in the analysis of supersonic flow.
Book Synopsis Stresses in and General Instability of Monocoque Cylinders with Cutouts by : Nicholas John Hoff
Download or read book Stresses in and General Instability of Monocoque Cylinders with Cutouts written by Nicholas John Hoff and published by . This book was released on 1949 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt: All but one cylinder failed in general instability. The one that did not show the general-instability pattern failed in tension.
Download or read book Report written by and published by . This book was released on 1945 with total page 620 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Verification of Two Methods for Computing the Take-off Ground Run of Propeller-driven Aircraft by : Welko E. Gasich
Download or read book Experimental Verification of Two Methods for Computing the Take-off Ground Run of Propeller-driven Aircraft written by Welko E. Gasich and published by . This book was released on 1947 with total page 606 pages. Available in PDF, EPUB and Kindle. Book excerpt: A comparison is presented between the measured take-off ground run of an airplane equipped with seven different propeller-engine gear-ratio combinations and the computed distances by two different methods.
Book Synopsis Pressure-distribution Measurements on the Rotating Blades of a Single-stage Axial-flow Compressor by : Jack F. Runckel
Download or read book Pressure-distribution Measurements on the Rotating Blades of a Single-stage Axial-flow Compressor written by Jack F. Runckel and published by . This book was released on 1947 with total page 550 pages. Available in PDF, EPUB and Kindle. Book excerpt: A preliminary investigation has been made of the pressure distribution about the mean-radius section of the rotating blades of a single-stage axial-flow compressor at a blade Mach number of 0.35. A 24-cell pressure-transfer device used in obtaining the pressure data is described and the accuracy of these data is established by several independent methods.
Download or read book Technical Note written by and published by . This book was released on 1946 with total page 680 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Selected Listing of NASA Scientific and Technical Reports for ... by :
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 750 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Velocity Distribution on Wing Sections of Arbitrary Shape in Compressible Potential Flow by : Lipman Bers
Download or read book Velocity Distribution on Wing Sections of Arbitrary Shape in Compressible Potential Flow written by Lipman Bers and published by . This book was released on 1946 with total page 630 pages. Available in PDF, EPUB and Kindle. Book excerpt: As a first step toward the computation of the velocity distribution along a wing profile of arbitrary shape in a compressible fluid, the circulation-free flow around a symmetrical profile is treated under the assumption of the simplified density-speed relation due to Tchaplygin, Karman, and Tsien. The velocity distribution problem is reduced to a nonlinear integral equation which is solved by a fairly rapidly convergent iteration method. Numerical examples are given.
Book Synopsis Investigation of Bonding Between Metals and Ceramics by : H. J. Hamjian
Download or read book Investigation of Bonding Between Metals and Ceramics written by H. J. Hamjian and published by . This book was released on 1949 with total page 696 pages. Available in PDF, EPUB and Kindle. Book excerpt: The experiments conducted with boron carbide and each of four metals showed that nickel, cobalt, and iron formed a bonding zone between the metal and the ceramic and that chromium showed satisfactory physical wetting characteristics on the ceramic.
Book Synopsis Fairing Compositions for Aircraft Surfaces by : Philip S. Turner
Download or read book Fairing Compositions for Aircraft Surfaces written by Philip S. Turner and published by . This book was released on 1944 with total page 738 pages. Available in PDF, EPUB and Kindle. Book excerpt: Fairing compositions are applied to aircraft surfaces, welds and junctions of metal plates, and rivet depressions to improve aerodynamic efficiency of the airplane at high speeds. A critical problem involved in their use is the maintenance of satisfactory adhesion to the metal under the extremes of temperature, weathering, and vibration encountered in service. This report describes tests which were developed to evaluate fairing compositions and presents the results of measurements with experimental mixtures of various plastics, fillers, and solvents. Important factors in obtaining satisfactory performance are low moisture absorption, a softening temperature no higher than the temperature of application, and a coefficient of thermal expansion at low temperatures equal to that of the metal.
Book Synopsis Aeronautical Engineering Review by :
Download or read book Aeronautical Engineering Review written by and published by . This book was released on 1957 with total page 1908 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Bearing Strengths of Some Wrought-aluminum Alloys by : R. L. Moore
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.
