Download or read book Experimental Investigation of Aerodynamic Effects of External Combustion in Airstream Below Two dimensional Supersonic Wing at Mach 2 5 and 3 0 written by Robert G. Dorsch and published by . This book was released on 1959 with total page 19 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Experimental Investigation of Aerodynamic Effects of External Combustion in Airstream Below 2 dimensional Supersonic Wing at Mach 2 5 and 3 0 with List of References written by and published by . This book was released on 1959 with total page 19 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of Aerodynamic Effects of External Combustion Below Flat plate Model in 10 by 10 foot Wind Tunnel at Mach 2 4 written by Robert G. Dorsch and published by . This book was released on 1960 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Note written by United States. National Aeronautics and Space Administration and published by . This book was released on 1961 with total page 442 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Progress in Aeronautical Sciences written by D. Küchemann and published by Elsevier. This book was released on 2016-07-02 with total page 442 pages. Available in PDF, EPUB and Kindle. Book excerpt: Progress in Aeronautical Sciences, Volume 8 is a collection of papers that covers the widening field of aeronautical sciences. The first article deals with problems in fluid mechanics and practical aerodynamics. This paper includes reducing problems to integral equations; the comparison of calculated results with exact analytic solutions; and with experimental pressure distributions using various configurations. The book follows this discussion with a review of the methods for designing swept-winged aircraft, including the design of a symmetrical-fuselage combination at zero incidence. The text also reviews the propulsion characteristics of a hypothetical aircraft flying at hypersonic speeds, and then focuses on air-breathing engines to power hypersonic aircrafts of which the scramjet is the most promising. The publication renders a comprehensive report on the viscous flow in boundary layers in ducts under rarefied conditions. The book then reviews investigations made on the viscous flow through tubes, both in continuum flow and in free-molecule flow. Another paper develops the fundamental mathematical and physical bases of magnetohydrodynamic flow through ducts in the presence of an applied electromagnetic field. Such review is useful when applied to electromagnetic flowmeters, pumps, or generators. The volume can be helpful for aerodynamic researchers, aviation technologists and designers, and aeronautical engineers.
Download or read book ARS Journal written by American Rocket Society and published by . This book was released on 1960 with total page 1254 pages. Available in PDF, EPUB and Kindle. Book excerpt: Supplements accompany some issues.
Download or read book Philosophical Transactions of the Royal Society of London written by and published by . This book was released on 1991 with total page 684 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Journal of the Aero space Sciences written by and published by . This book was released on 1960 with total page 1002 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of the Effects of Model Scale and Stream Reynolds Number on the Aerodynamic Characteristics of Two Rectangular Wings at Supersonic Speeds on the Langley 9 inch Supersonic Tunnel written by Donald E. Coletti and published by . This book was released on 1955 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Experimental Investigation of a Mach 5 Isentropic Spike Inlet at and Below Design Speed written by Leonard E. Stitt and published by . This book was released on 1959 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Exploratory Investigation of Aerodynamic Effects of External Combustion of Aluminum Borohydride in Airstream Adjacent to Flat Plate in Mach 2 46 Tunnel written by Robert G. Dorsch and published by . This book was released on 1957 with total page 91 pages. Available in PDF, EPUB and Kindle. Book excerpt: Pressure distributions associated with stable combustion of aluminum borohydride in the supersonic stream adjacent to a short, 13-inch chord, and an extended, 25-inch chord, flat-plate model were determined experimentally. The models were mounted in the center of the test section of a 1- by 1-foot Mach 2.46 wind tunnel. High-speed direct and schlieren motion pictures of the flame and associated shock waves were taken, and selected photographs are presented.
Download or read book Experimental Investigation of Wing Installation Effects on a Two Dimensional Mixer Ejector Nozzle for Supersonic Transport Aircraft written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-03 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: Experimental results from a wind tunnel test conducted to investigate propulsion/airframe integration (PAI) effects are presented. The objectives of the test were to examine rough order-of-magnitude changes in the acoustic characteristics of a mixer/ejector nozzle due to the presence of a wing and to obtain limited wing and nozzle flow-field measurements. A simple representative supersonic transport wing planform, with deflecting flaps, was installed above a two-dimensional mixer/ejector nozzle that was supplied with high-pressure heated air. Various configurations and wing positions with respect to the nozzle were studied. Because of hardware problems, no acoustics and only a limited set of flow-field data were obtained. For most hardware configurations tested, no significant propulsion/airframe integration effects were identified. Significant effects were seen for extreme flap deflections. The combination of the exploratory nature of the test and the limited flow-field instrumentation made it impossible to identify definitive propulsion/airframe integration effects. Anderson, David J. and Lambert, Heather H. and Mizukami, Masashi Glenn Research Center RTOP 537-02-23...
Download or read book AN EXPERIMENTAL AND THEORETICAL INVESTIGATION OF TWO DIMENSIONAL JET FLAP AERODYNAMIC AT SUPERSONIC SPEEDS written by Norman E. Hawk and Jumea.L. Amick and published by . This book was released on 1965 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book List of Selected References on NASA Programs written by Library of Congress. Science and Technology Division and published by . This book was released on 1962 with total page 244 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book International Aerospace Abstracts written by and published by . This book was released on 1996 with total page 940 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Optical Study of Sonic and Supersonic Jet Penetration from a Flat Plate Into a Mach 2 Airstream written by Martin Hersch and published by . This book was released on 1970 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind Tunnel Tests of Supersonic Two dimensional and Half axisymmetric Inlet Models in a Nonuniform Flow Field at Mach Numbers from 1 5 Through 2 5 written by Frederick K. Hube and published by . This book was released on 1971 with total page 274 pages. Available in PDF, EPUB and Kindle. Book excerpt:
