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Numerical Computation Of Intermediate Altitude Rocket Exhaust Plumes Including Nonequilibrium Chemical Reactions And Diffusion
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Book Synopsis Numerical Computation of Intermediate Altitude Rocket Exhaust Plumes, Including Nonequilibrium Chemical Reactions and Diffusion by : John. C. Tannehill
Download or read book Numerical Computation of Intermediate Altitude Rocket Exhaust Plumes, Including Nonequilibrium Chemical Reactions and Diffusion written by John. C. Tannehill and published by . This book was released on 1969 with total page 470 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1983 with total page 1368 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Iowa State College Journal of Science by :
Download or read book Iowa State College Journal of Science written by and published by . This book was released on 1970 with total page 1236 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Theory on Afterburning in a Low-altitude Rocket Exhaust Plume by : Richard Shao-Lin Lee
Download or read book Theory on Afterburning in a Low-altitude Rocket Exhaust Plume written by Richard Shao-Lin Lee and published by . This book was released on 1968 with total page 59 pages. Available in PDF, EPUB and Kindle. Book excerpt: An improved aerodynamic model is proposed for the exhaust plume issuing from a low-altitude rocket nozzle exit into quiescent ambient air in which chemical reactions and compressibility predominate. The model is based on the presently available knowledge and established aerodynamic principles for the various flow regimes involved. The major assumptions made are individually substantiated by related experimental evidence in existing literature. A theoretical analysis is carried over the whole flow region based on the Karman's integral approach to find solutions for the gross aerodynamic and thermodynamic behavior of the plume. Theory incorporating on empirically derived constants provides the required radial distribution function for the integration. Solutions are obtained for the velocity, density, temperature and chemical composition fields for extended regions of the plume. These results will provide the much needed framework for the understanding of the elements which contribute to the phenomenon of radar attenuation of rocket exhaust plumes. (Author).
Download or read book Iowa State Journal of Science written by and published by . This book was released on 1970 with total page 1224 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Annual Report of the Institute of Physics, Academia Sinica by :
Download or read book Annual Report of the Institute of Physics, Academia Sinica written by and published by . This book was released on 1983 with total page 1256 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Research in Progress written by and published by . This book was released on 1991 with total page 274 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Solid Rocket Exhaust in the Stratosphere by : M. R. Denison
Download or read book Solid Rocket Exhaust in the Stratosphere written by M. R. Denison and published by . This book was released on 1992 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :Frederick S. Simmons Publisher :AIAA (American Institute of Aeronautics & Astronautics) ISBN 13 : Total Pages :312 pages Book Rating :4.3/5 (91 download)
Book Synopsis Rocket Exhaust Plume Phenomenology by : Frederick S. Simmons
Download or read book Rocket Exhaust Plume Phenomenology written by Frederick S. Simmons and published by AIAA (American Institute of Aeronautics & Astronautics). This book was released on 2000 with total page 312 pages. Available in PDF, EPUB and Kindle. Book excerpt: This new book deals with the phenomenology of rocket exhaust plumes as the targets of space-based surveillance systems. Topics include the physical and chemical processes in rocket engines and their exhaust plumes, particularly in regard to flow properties, gas dynamics, and radiative mechanisms that are responsible for the generation of emission in rocket exhaust plumes at infrared and other wavelengths. System designers in a number of defense-related areas will be able to put the information in this book to immediate use.
Book Synopsis MOC Computation of Intermediate-altitude Rocket Plumes with Shock Waves by : L. Genkin
Download or read book MOC Computation of Intermediate-altitude Rocket Plumes with Shock Waves written by L. Genkin and published by . This book was released on 1996 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Study of Rocket Exhaust Plumes Using a One-dimensional Flow Model with Nonequilibrium Chemistry by : Edwin Cash Word
Download or read book A Study of Rocket Exhaust Plumes Using a One-dimensional Flow Model with Nonequilibrium Chemistry written by Edwin Cash Word and published by . This book was released on 1977 with total page 114 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis High Altitude Rocket Plume Structure: Experiment and Calculations by : Frederick P. Boynton
Download or read book High Altitude Rocket Plume Structure: Experiment and Calculations written by Frederick P. Boynton and published by . This book was released on 1972 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: Values of impact pressure and species number density measured in a wind tunnel experiment simulating a high-altitude rocket exhaust plume are compared with values calculated with a computer code. Considering a number of uncertainties in the absolute calibrations of the experiment, agreement is generally considered satisfactory for conditions in the mixing region between plume and free stream gases. However, in the forward part of the plume, the data suggests that free-stream gas penetrates further into the plume than the calculation predicts; the cause of this discrepancy is unknown. (Author).
Book Synopsis Numerical Calculations of Viscous High-Altitude Exhaust Plume Flow Fields by : Frederick P. Boynton
Download or read book Numerical Calculations of Viscous High-Altitude Exhaust Plume Flow Fields written by Frederick P. Boynton and published by . This book was released on 1970 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report describes the results of exhaust plume flow field computations at ionospheric altitudes. Viscous transport, including multicomponent and pressure diffusion, is included in the plume-atmosphere shock layer. The shocks are treated as discontinuities across which the Rankine-Hugoniot relations are applied. The intent of the calculations is to provide detailed composition and temperature distributions in the entire flow from the high temperature bow region to the trailing Mach disc region. (Author).
Book Synopsis Rocket Plume Radiance. Volume Vi. Calculation of Power from a Rocket Exhaust Plume as a Function of Altitude by : John T. Neu
Download or read book Rocket Plume Radiance. Volume Vi. Calculation of Power from a Rocket Exhaust Plume as a Function of Altitude written by John T. Neu and published by . This book was released on 1960 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt: The results of computation of the power available from a rocket plume are given. A simplified model was used which assumes the sequential occurrence of exhaust gases expansion to ambient pressure, interaction with the atmosphere, and finally dissipation of power. It is suggested that the experimentally determined drop in radiation at about 180,000 feet is probably due to a power limitation and cessation of afterburning. Power available above about 180,000 feet is due to emission phenomena occurring before the plume equilibrates (expands, etc.) with the ambient atmosphere. It is noted that no fundamental reason exists for expecting missile thrust as a function of altitude to correlate with rocket radiance. A correlation of radiance from different missiles at a given altitude vs thrust has some theoretical justification, however, propellant flow rate is suggested as a better quantity than thrust for this correlation. (Author).
Book Synopsis Analysis and Correlation of High Altitude Rocket Exhaust Plume Experimental Data by : Larry R. Ring
Download or read book Analysis and Correlation of High Altitude Rocket Exhaust Plume Experimental Data written by Larry R. Ring and published by . This book was released on 1973 with total page 107 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results are presented of a study for evaluating the applicability and accuracy of rocket motor and exhaust plume gasdynamic analytical models. Evaluation of these analytical models was based upon correlation of analytical predictions with experimental data obtained in the High Altitude Plume Radiation Program. The effects of oxidizer-to-fuel ratio gradients, combustion efficiency, combustion chamber mixing, nozzle throat expansion and chemistry model were ascertained. Non-continuum effects and closed form analytical techniques were also considered. (Modified author abstract).
Book Synopsis Numerical Simulation of Chemical Reactions in Point-source Plumes by : John Peter Meeder
Download or read book Numerical Simulation of Chemical Reactions in Point-source Plumes written by John Peter Meeder and published by . This book was released on 1998 with total page 105 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Comprehensive Dissertation Index, 1861-1972: Engineering: general and aeronautical by : Xerox University Microfilms
Download or read book Comprehensive Dissertation Index, 1861-1972: Engineering: general and aeronautical written by Xerox University Microfilms and published by . This book was released on 1973 with total page 906 pages. Available in PDF, EPUB and Kindle. Book excerpt:
