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Author : N. J. Hoff
Publisher :
ISBN 13 :
Total Pages : 206 pages
Book Rating : 4.3/5 (91 download)
Download or read book Induction Heating and Theory in the Solution of Transient Problems of Aircraft Structures written by N. J. Hoff and published by . This book was released on 1956 with total page 206 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 442 pages
Book Rating : 4.3/5 (243 download)
Download or read book U.S. Government Research Reports written by and published by . This book was released on 1957 with total page 442 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : United States. National Advisory Committee for Aeronautics
Publisher :
ISBN 13 :
Total Pages : 1160 pages
Book Rating : 4.E/5 ( download)
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 1958 with total page 1160 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 1908 pages
Book Rating : 4.3/5 (91 download)
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:
Author : Nicholas John Hoff
Publisher : Pergamon
ISBN 13 :
Total Pages : 330 pages
Book Rating : 4.F/5 ( download)
Download or read book Aerostructures; Selected Papers of Nicholas J. Hoff written by Nicholas John Hoff and published by Pergamon. This book was released on 1971 with total page 330 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Alton P. Mayo
Publisher :
ISBN 13 :
Total Pages : 632 pages
Book Rating : 4.F/5 ( download)
Download or read book Matrix Method for Obtaining Spanwise Moments and Deflections of Torsionally Rigid Rotor Blades with Arbitrary Loadings written by Alton P. Mayo and published by . This book was released on 1958 with total page 632 pages. Available in PDF, EPUB and Kindle. Book excerpt: A matrix solution for the spanwise bending moments and deflections of a torsionally rigid rotor blade subjected to an arbitrary loading is presented. The method includes the cantilever, teetering, and hinged blades in hovering and in steady forward flight. The method is comparatively short, involves only standard matrix procedures, and does not require that the mode shapes or natural frequencies be known.
Author : Nicholas John Hoff
Publisher :
ISBN 13 :
Total Pages : 370 pages
Book Rating : 4.3/5 (91 download)
Download or read book Theory and Experiment in the Solution of Structural Problems of Supersonic Aircraft written by Nicholas John Hoff and published by . This book was released on 1956 with total page 370 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : John R. Malcom
Publisher :
ISBN 13 :
Total Pages : 204 pages
Book Rating : 4.3/5 (91 download)
Download or read book Comparison of Relative Costs of Thermal Analysis Methods for Hypersonic Vehicle Compartments written by John R. Malcom and published by . This book was released on 1961 with total page 204 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 218 pages
Book Rating : 4.3/5 (243 download)
Download or read book Business Service Check List written by and published by . This book was released on 1957 with total page 218 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Society for Experimental Stress Analysis
Publisher :
ISBN 13 :
Total Pages : 264 pages
Book Rating : 4.3/5 (97 download)
Download or read book Proceedings of the Society for Experimental Stress Analysis written by Society for Experimental Stress Analysis and published by . This book was released on 1976 with total page 264 pages. Available in PDF, EPUB and Kindle. Book excerpt: Vol. 1, no. 1 contains Proceedings of the 17th (or the last) Eastern Photoelasticity Conference.
Author : Polytechnic Institute of Brooklyn
Publisher :
ISBN 13 :
Total Pages : 108 pages
Book Rating : 4.:/5 (319 download)
Download or read book Staff publication written by Polytechnic Institute of Brooklyn and published by . This book was released on 1958 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Stanford University. Department of Aeronautics and Astronautics
Publisher :
ISBN 13 :
Total Pages : 86 pages
Book Rating : 4.F/5 ( download)
Download or read book Thermal Buckling of Thin-walled Circular Cylindrical Shells written by Stanford University. Department of Aeronautics and Astronautics and published by . This book was released on 1962 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Zbigniew Krzywoblocki (|d)
Publisher :
ISBN 13 :
Total Pages : 170 pages
Book Rating : 4.3/5 (91 download)
Download or read book Aerodynamic Studies written by Zbigniew Krzywoblocki (|d) and published by . This book was released on 1957 with total page 170 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Polytechnic Institute of Brooklyn
Publisher :
ISBN 13 :
Total Pages : 118 pages
Book Rating : 4.3/5 (91 download)
Download or read book Staff Publications written by Polytechnic Institute of Brooklyn and published by . This book was released on 1956 with total page 118 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : National Aeronaut Administration (Nasa)
Publisher :
ISBN 13 :
Total Pages : 56 pages
Book Rating : 4.6/5 (743 download)
Download or read book Analysis and Sizing for Transient Thermal Heating of Insulated Aerospace Vehicle Structures written by National Aeronaut Administration (Nasa) and published by . This book was released on 2020-08-18 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt: An analytical solution was derived for the transient response of an insulated structure subjected to a simplified heat pulse. The solution is solely a function of two nondimensional parameters. Simpler functions of these two parameters were developed to approximate the maximum structural temperature over a wide range of parameter values. Techniques were developed to choose constant, effective thermal properties to represent the relevant temperature and pressure-dependent properties for the insulator and structure. A technique was also developed to map a time-varying surface temperature history to an equivalent square heat pulse. Equations were also developed for the minimum mass required to maintain the inner, unheated surface below a specified temperature. In the course of the derivation, two figures of merit were identified. Required insulation masses calculated using the approximate equation were shown to typically agree with finite element results within 10%-20% over the relevant range of parameters studied. Blosser, Max L. Langley Research Center NASA/TP-2012-217595, L-20165, NF1676L-15092 AEROSPACE VEHICLES; INSULATION; TRANSIENT HEATING; AIRCRAFT STRUCTURES; TRANSIENT RESPONSE; MATHEMATICAL MODELS; HYPERSONIC VEHICLES; SIZE (DIMENSIONS); FINITE ELEMENT METHOD; TEMPERATURE DEPENDENCE; THERMAL PROTECTION; SURFACE TEMPERATURE
Author :
Publisher :
ISBN 13 :
Total Pages : 1434 pages
Book Rating : 4.:/5 (319 download)
Download or read book Industrial Laboratories written by and published by . This book was released on 1958 with total page 1434 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 1010 pages
Book Rating : 4.3/5 (91 download)
Download or read book Bibliography of Scientific and Industrial Reports written by and published by . This book was released on 1957 with total page 1010 pages. Available in PDF, EPUB and Kindle. Book excerpt:
