Download or read book Notes for a Special Summer Program in Aerodynamic Heating of Aircraft Structures in High speed Flight June 25 July 6 1956 written by Massachusetts Institute of Technology. Department of Aeronautics and Astronautics and published by . This book was released on 1956 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Notes for a Special Summer Program in Aerodynamic Heating of Aircraft Structures in High speed Flight June 25 July 6 1956 written by Massachusetts Institute of Technology and published by . This book was released on 1956 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Notes for a Special Summer Program in Aerodynamic Heating of Aircraft Structures in High speed Flight written by Massachusetts Institute of Technology. Department of Aeronautics and Astronautics and published by . This book was released on 1956 with total page 670 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Notes for a special summer program in aerodynamic heating of aircraft structures written by Massachusetts Institute of Technology and published by . This book was released on 1956 with total page 5 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 1962 with total page 612 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Handbook of Military Infrared Technology 1965 written by United States. Naval Research Office and published by . This book was released on 1966 with total page 922 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Proceedings of Symposium on Aerothermoelasticity written by David M. Jones and published by . This book was released on 1962 with total page 1028 pages. Available in PDF, EPUB and Kindle. Book excerpt: A symposium on Aerothermoelasticity was held to present the latest significant developments in each scientific area and engineering area that comprise the component parts of this technology. New and significant contributions were presented in four technical areas consisting of dynamic aerothermoelasticity (flutter), stability and control, thermodynamics and aerodynamics (or aerothermodynamics), and structures including material and construction concepts. Categories important and significant to each technical area are discussed state-of-the-art wise. In addition, 26 separate papers are given on items of special importance.
Download or read book Proceedings of the 3rd Symposium on High Speed Aerodynamics and Structures written by and published by . This book was released on 1958 with total page 336 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Method for Calculating Transient Surface Temperatures and Surface Heating Rates for High speed Aircraft written by Robert D. Quinn and published by . This book was released on 2000 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report describes a method that can calculate transient aerodynamic heating and transient surface temperatures at supersonic and hypersonic speeds. This method can rapidly calculate temperature and heating rate time-histories for complete flight trajectories. Semi-empirical theories are used to calculate laminar and turbulent heat transfer coefficients and a procedure for estimating boundary-layer transition is included. Results from this method are compared with flight data from the X-15 research vehicle, YF-12 airplane, and the Space Shuttle Orbiter. These comparisons show that the calculated values are in good agreement with the measured flight data.
Download or read book Thermal Structures and Materials for High speed Flight written by Earl Arthur Thornton and published by AIAA (American Institute of Aeronautics & Astronautics). This book was released on 1992 with total page 576 pages. Available in PDF, EPUB and Kindle. Book excerpt: This text presents recent research and development in aerothermodynamics, advanced light metals and composites, thermal structures, materials performance and failure criteria, and intelligent processing of materials, as they relate to high-speed flight. Researchers and designers of aerospace vehicles for high-speed flight, as well as materials scientists, should find this text valuable.
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 1957 with total page 218 pages. Available in PDF, EPUB and Kindle. Book excerpt: Vol. 1, no. 1 contains Proceedings of the 17th (or the last) Eastern Photoelasticity Conference.
Download or read book ASD Technical Report written by and published by . This book was released on 1962 with total page 1038 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book International Series of Monographs in Aeronautics and Astronautics written by and published by . This book was released on 1961 with total page 368 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Report written by Tōkyō Daigaku. Kōkū Kenkyūjo and published by . This book was released on 1960 with total page 300 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Effects of Aerodynamic Heating and Heat Transfer on the Surface Temperature of a Body of Revolution in Steady Supersonic Flight written by Richard Scherrer and published by . This book was released on 1947 with total page 542 pages. Available in PDF, EPUB and Kindle. Book excerpt: An approximate method for determining the convective cooling requirement in the laminar-boundary-layer region of a body of revolution in high-speed flight was developed and applied to an example body. The cooling requirement for the example body was determined as a function of Mach number, altitude, size, and a surface-temperature parameter. The maximum value of Mach number considered was 3.0 and the altitudes considered were those within the lower constant-temperature region of the atmosphere (40,000 to 120,000 ft). The extent of the laminar boundary layer was determined approximately at each condition as a function of the variables considered.
Download or read book Reports written by Tōkyō Daigaku Uchu Kagaku Kōkugaku Kenkyujo and published by . This book was released on 1960 with total page 550 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Current Papers written by Aeronautical Research Council (Great Britain) and published by . This book was released on 1962 with total page 720 pages. Available in PDF, EPUB and Kindle. Book excerpt:
