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Heat Transfer In Rocket Engines
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Book Synopsis Heat Transfer in Rocket Engines by : H. Ziebland
Download or read book Heat Transfer in Rocket Engines written by H. Ziebland and published by . This book was released on 1971 with total page 172 pages. Available in PDF, EPUB and Kindle. Book excerpt: In the first part of this book the various basic heat transfer processes are considered, -- simple convective heat transfer from hot gases to the engine walls under various conditions, radiation heat transfer, and coolant heat transfer processes. This part is followed by one describing the various methods of cooling used in liquid propellant rocket engines, such as regenerative, film, ablation and radiation cooling. The final part concerns the properties of materials that will have to be known by the engine designer, from the transport properties of the hot combustion gases to those of the materials from which the engine will be constructed. Emphasis was placed on presenting simple methods for calculating the magnitude of heat transfer rather than providing the most modern and rigorous theories, particularly in the field of developing boundary layers. (Author).
Book Synopsis Analysis of the Transient Radiation Heat Transfer of an Uncooled Rocket Engine Operating Outside Earth's Atmosphere by : William H. Robbins
Download or read book Analysis of the Transient Radiation Heat Transfer of an Uncooled Rocket Engine Operating Outside Earth's Atmosphere written by William H. Robbins and published by . This book was released on 1959 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Analysis of Effects of Rocket-engine Design Parameters on Regenerative-cooling Capabilities of Several Propellants by : Arthur N. Curren
Download or read book Analysis of Effects of Rocket-engine Design Parameters on Regenerative-cooling Capabilities of Several Propellants written by Arthur N. Curren and published by . This book was released on 1959 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Application of Various Techniques for Determining Local Heat-transfer Coefficients in a Rocket Engine from Transient Experimental Data by : Curt H. Liebert
Download or read book Application of Various Techniques for Determining Local Heat-transfer Coefficients in a Rocket Engine from Transient Experimental Data written by Curt H. Liebert and published by . This book was released on 1960 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Heat-transfer Study of a Regeneratively Cooled Hydrogen-fluorine Rocket Engine at Low Chamber Pressure by :
Download or read book Experimental Heat-transfer Study of a Regeneratively Cooled Hydrogen-fluorine Rocket Engine at Low Chamber Pressure written by and published by . This book was released on 1967 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Internal Combustion Processes of Liquid Rocket Engines by : Zhen-Guo Wang
Download or read book Internal Combustion Processes of Liquid Rocket Engines written by Zhen-Guo Wang and published by John Wiley & Sons. This book was released on 2016-05-17 with total page 396 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book concentrates on modeling and numerical simulations of combustion in liquid rocket engines, covering liquid propellant atomization, evaporation of liquid droplets, turbulent flows, turbulent combustion, heat transfer, and combustion instability. It presents some state of the art models and numerical methodologies in this area. The book can be categorized into two parts. Part 1 describes the modeling for each subtopic of the combustion process in the liquid rocket engines. Part 2 presents detailed numerical methodology and several representative applications in simulations of rocket engine combustion.
Book Synopsis Convective Heat Transfer in Rocket Engines by : R. C. Parkinson
Download or read book Convective Heat Transfer in Rocket Engines written by R. C. Parkinson and published by . This book was released on 1968 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Hot-gas-side Heat Transfer Characteristics of Subscale, Plug-nozzle Rocket Calorimeter Chamber by : Richard J. Quentmeyer
Download or read book Hot-gas-side Heat Transfer Characteristics of Subscale, Plug-nozzle Rocket Calorimeter Chamber written by Richard J. Quentmeyer and published by . This book was released on 1993 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Heat Transfer in Rocket Engines by : AGARD.
Download or read book Heat Transfer in Rocket Engines written by AGARD. and published by . This book was released on 1971 with total page 154 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Variation of Convective Heat-transfer Coefficient Around a Simulated Rocket Cooling Tube Section by : Ronald G. Huff
Download or read book Variation of Convective Heat-transfer Coefficient Around a Simulated Rocket Cooling Tube Section written by Ronald G. Huff and published by . This book was released on 1969 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Fast Reactor Rocket Engines--heat Transfer by : Ralph Sherman Cooper
Download or read book Fast Reactor Rocket Engines--heat Transfer written by Ralph Sherman Cooper and published by . This book was released on 1962 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Modern Engineering for Design of Liquid-Propellant Rocket Engines by : Dieter K. Huzel
Download or read book Modern Engineering for Design of Liquid-Propellant Rocket Engines written by Dieter K. Huzel and published by AIAA. This book was released on 1992 with total page 452 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Convective Heat Transfer in Rocket Engines by : R. C. Parkinson
Download or read book Convective Heat Transfer in Rocket Engines written by R. C. Parkinson and published by . This book was released on 1967 with total page 51 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Heat Transfer to a Sphere with a Retrorocket Exhausting Into a Free Stream by : Robert A. Wasko
Download or read book Heat Transfer to a Sphere with a Retrorocket Exhausting Into a Free Stream written by Robert A. Wasko and published by . This book was released on 1962 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Heat Transfer in Rocket Engines by : Theodore M. Long
Download or read book Heat Transfer in Rocket Engines written by Theodore M. Long and published by . This book was released on 1948 with total page 90 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722267384 Total Pages :34 pages Book Rating :4.2/5 (673 download)
Book Synopsis Heat Transfer to Throat Tubes in a Square-Chambered Rocket Engine at the NASA Lewis Research Center by : National Aeronautics and Space Administration (NASA)
Download or read book Heat Transfer to Throat Tubes in a Square-Chambered Rocket Engine at the NASA Lewis Research Center written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-05 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: A gaseous H2/O2 rocket engine was constructed at the NASA-Lewis to provide a high heat flux source representative of the heat flux to the blades in the high pressure fuel turbopump (HPFTP) during startup of the space shuttle main engines. The high heat flux source was required to evaluate the durability of thermal barrier coatings being investigated for use on these blades. The heat transfer, and specifically, the heat flux to tubes located at the throat of the test rocket engine was evaluated and compared to the heat flux to the blades in the HPFTP during engine startup. Gas temperatures, pressures and heat transfer coefficients in the test rocket engine were measured. Near surface metal temperatures below thin thermal barrier coatings were also measured at various angular orientations around the throat tube to indicate the angular dependence of the heat transfer coefficients. A finite difference model for a throat tube was developed and a thermal analysis was performed using the measured gas temperatures and the derived heat transfer coefficients to predict metal temperatures in the tube. Near surface metal temperatures of an uncoated throat tube were measured at the stagnation point and showed good agreement with temperatures predicted by the thermal model. The maximum heat flux to the throat tube was calculated and compared to that predicted for the leading edge of an HPFTP blade. It is shown that the heat flux to an uncooled throat tube is slightly greater than the heat flux to an HPFTP blade during engine startup. Nesbitt, James A. and Brindley, William J. Glenn Research Center RTOP 505-63-1A...
Book Synopsis Rocket Propulsion Elements by : George P. Sutton
Download or read book Rocket Propulsion Elements written by George P. Sutton and published by Wiley-Interscience. This book was released on 1992-05-07 with total page 658 pages. Available in PDF, EPUB and Kindle. Book excerpt: Concentrates on the subject of rock propulsion, its basic technology, performance and design rationale. Provides an introduction to the subject, an understanding of basic principles, a description of their physical mechanisms and designs, and an understanding of the application of rocket propulsion to flying vehicles.
