Download or read book Response of Structures to Aircraft Generated Shock Waves written by and published by . This book was released on 1959 with total page 158 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book RESPONSE OF STRUCTURES TO AIRCRAFT GENERATED SHOCK WAVES written by and published by . This book was released on 1959 with total page 125 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Shock Wave Boundary Layer Interactions written by Holger Babinsky and published by Cambridge University Press. This book was released on 2011-09-12 with total page 481 pages. Available in PDF, EPUB and Kindle. Book excerpt: Shock wave-boundary-layer interaction (SBLI) is a fundamental phenomenon in gas dynamics that is observed in many practical situations, ranging from transonic aircraft wings to hypersonic vehicles and engines. SBLIs have the potential to pose serious problems in a flowfield; hence they often prove to be a critical - or even design limiting - issue for many aerospace applications. This is the first book devoted solely to a comprehensive, state-of-the-art explanation of this phenomenon. It includes a description of the basic fluid mechanics of SBLIs plus contributions from leading international experts who share their insight into their physics and the impact they have in practical flow situations. This book is for practitioners and graduate students in aerodynamics who wish to familiarize themselves with all aspects of SBLI flows. It is a valuable resource for specialists because it compiles experimental, computational and theoretical knowledge in one place.

Download or read book High Altitude Shock Wave Structure written by S. M. Scala and published by . This book was released on 1962 with total page 136 pages. Available in PDF, EPUB and Kindle. Book excerpt: Part 2. : This investigation was undertaken with two primary objectives. The first objective was to see if chemical reaction rates can be determined to about the same accuracy behind combustion driven shock waves as that previously attained behind shock waves generated by high pressure hydrogen or helium. The second was to obtain chemical rate data for nitrogen.

Download or read book The Effects of Sonic Boom and Similar Impulsive Noise on Strcutures written by United States. Environmental Protection Agency and published by . This book was released on 1971 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Program to Induce High Blast induced Airloads and Structural Response of Lifting Surfaces written by R. L. Jarvis and published by . This book was released on 1964 with total page 521 pages. Available in PDF, EPUB and Kindle. Book excerpt: Six experiments were conducted to measure the transient character of the airloads induced by the interaction of blast generated shock waves on a moving airfoil. The tests were conducted on a rigid (airloads) model of swept planform, similar in type to a B47/B52 aircraft. Airfoil motion was simulated by the shock tube which produced a jet flow of Mach 0.7. Shock waves were generated by explosive charges which were varied in sized and proximity to obtain airloads on the wing that changed both the angle of attack and blast duration through a range from small to large. The wing specimens were heavily instrumented with pressure transducers to measure the time history of the variation in the airloads. Response of the wing to the airloads was measured by strain gages and accelerometers. Pressure instrumentation was also used to measure the character of the blast environment. Blast parameters were varied to obtain induced airloads with nominal values for the angle of attack of 8, 20 and 30 degrees. At each of these angles of attack, an experiment was run with a short and long duration shock wave to study the effect of decay rate on the airloads. (Author).

Download or read book The Effects of Sonic Boom and Similar Impulsive Noise on Structures written by United States. National Bureau of Standards and published by . This book was released on 1971 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 702 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book NASA Reference Publication written by and published by . This book was released on 1977 with total page 628 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book High Speed Research Sonic Boom Volume 1 written by and published by . This book was released on 1992 with total page 208 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Air Force Research Resum s written by and published by . This book was released on with total page 854 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Bibliography on Aeromedical Research with Abstracts written by Aerospace Medical Laboratory (U.S.) and published by . This book was released on 1960 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Explosively Generated Air Pressure Waves for Structural Forcing written by M. J. Harper and published by . This book was released on 1969 with total page 10 pages. Available in PDF, EPUB and Kindle. Book excerpt: The aerial blast wave generated by a small explosion may be used to produce impulsive forcing of structures with natural periods longer than approximately 1 msec; the free response of such structures may then be determined. A technique has been developed using spatial distributions of explosive whereby it is possible to generate waves of much longer durations and of a much wider range of shapes, so that studies of the forced response of structures are made feasible. The technique has been applied to the generation of a blast waveform of the same shape as that of the sonic bang, for example, thus permitting studies of response to sonic bangs to be carried out without the necessity of flying supersonic aircraft and without recourse to scaled model experiments. (Author).

Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1974 with total page 628 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Aeroacoustics of Flight Vehicles Noise sources written by Harvey H. Hubbard and published by . This book was released on 1991 with total page 612 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book The Performance Concept written by John P. Eberhard and published by . This book was released on 1969 with total page 206 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Aeroacoustics of Flight Vehicles written by Harvey H. Hubbard and published by . This book was released on 1991 with total page 620 pages. Available in PDF, EPUB and Kindle. Book excerpt: