Design of a Film Cooling Experiment for Rocket Engines

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ISBN 13 :
Total Pages : 266 pages
Book Rating : 4.:/5 (655 download)

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Book Synopsis Design of a Film Cooling Experiment for Rocket Engines by : Andrew L. Sincock

Download or read book Design of a Film Cooling Experiment for Rocket Engines written by Andrew L. Sincock and published by . This book was released on 2010 with total page 266 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Film Cooling Design Criteria for Small Rocket Engines

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ISBN 13 :
Total Pages : 16 pages
Book Rating : 4.:/5 (455 download)

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Book Synopsis Film Cooling Design Criteria for Small Rocket Engines by : R. Carl Stechman

Download or read book Film Cooling Design Criteria for Small Rocket Engines written by R. Carl Stechman and published by . This book was released on 1968 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Validation of Supersonic Film Cooling Modeling for Liquid Rocket Engine Applications

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Publisher : BiblioGov
ISBN 13 : 9781289142391
Total Pages : 58 pages
Book Rating : 4.1/5 (423 download)

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Book Synopsis Validation of Supersonic Film Cooling Modeling for Liquid Rocket Engine Applications by : Christopher I. Morris

Download or read book Validation of Supersonic Film Cooling Modeling for Liquid Rocket Engine Applications written by Christopher I. Morris and published by BiblioGov. This book was released on 2013-06 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt: Topics include: upper stage engine key requirements and design drivers; Calspan "stage 1" results, He slot injection into hypersonic flow (air); test articles for shock generator diagram, slot injector details, and instrumentation positions; test conditions; modeling approach; 2-d grid used for film cooling simulations of test article; heat flux profiles from 2-d flat plate simulations (run #4); heat flux profiles from 2-d backward facing step simulations (run #43); isometric sketch of single coolant nozzle, and x-z grid of half-nozzle domain; comparison of 2-d and 3-d simulations of coolant nozzles (run #45); flowfield properties along coolant nozzle centerline (run #45); comparison of 3-d CFD nozzle flow calculations with experimental data; nozzle exit plane reduced to linear profile for use in 2-d film-cooling simulations (run #45); synthetic Schlieren image of coolant injection region (run #45); axial velocity profiles from 2-d film-cooling simulation (run #45); coolant mass fraction profiles from 2-d film-cooling simulation (run #45); heat flux profiles from 2-d film cooling simulations (run #45); heat flux profiles from 2-d film cooling simulations (runs #47, #45, and #47); 3-d grid used for film cooling simulations of test article; heat flux contours from 3-d film-cooling simulation (run #45); and heat flux profiles from 3-d and 2-d film cooling simulations (runs #44, #46, and #47).

An Experimental and Theoretical Investigation of Film Cooling in Rocket Motors

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ISBN 13 :
Total Pages : 1 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis An Experimental and Theoretical Investigation of Film Cooling in Rocket Motors by : A. R. GRAHAM

Download or read book An Experimental and Theoretical Investigation of Film Cooling in Rocket Motors written by A. R. GRAHAM and published by . This book was released on 1957 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Modern Engineering for Design of Liquid-Propellant Rocket Engines

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Publisher : AIAA
ISBN 13 : 9781600864001
Total Pages : 452 pages
Book Rating : 4.8/5 (64 download)

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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:

Experimental Investigation of the Effectiveness of an Ablation-produced Film in Cooling a Rocket Nozzle

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ISBN 13 :
Total Pages : 22 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Experimental Investigation of the Effectiveness of an Ablation-produced Film in Cooling a Rocket Nozzle by : Richard R. Cullom

Download or read book Experimental Investigation of the Effectiveness of an Ablation-produced Film in Cooling a Rocket Nozzle written by Richard R. Cullom and published by . This book was released on 1961 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:

An Experimental and Technical Investigation of Film Cooling in Rocket Motors

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Publisher :
ISBN 13 :
Total Pages : 520 pages
Book Rating : 4.:/5 (249 download)

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Book Synopsis An Experimental and Technical Investigation of Film Cooling in Rocket Motors by : A. R. Graham

Download or read book An Experimental and Technical Investigation of Film Cooling in Rocket Motors written by A. R. Graham and published by . This book was released on 1957 with total page 520 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Proceedings of the 1st International Conference on Fluid, Thermal and Energy Systems

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Publisher : Springer Nature
ISBN 13 : 981995990X
Total Pages : 840 pages
Book Rating : 4.8/5 (199 download)

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Book Synopsis Proceedings of the 1st International Conference on Fluid, Thermal and Energy Systems by : Sudev Das

Download or read book Proceedings of the 1st International Conference on Fluid, Thermal and Energy Systems written by Sudev Das and published by Springer Nature. This book was released on 2024-01-17 with total page 840 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book comprises the proceedings of the 1st International Conference on Fluid, Thermal and Energy Systems. The contents of this book focus on phase change heat transfer, advanced energy systems, separated flows, turbulence and multi-phase modeling, computational fluid flow and heat transfer, thermal energy storage systems, integrated energy systems, nuclear thermal hydraulics, heat transfer in nanofluids, etc. This book serves as a useful reference to researchers, academicians, and students interested in the broad field of thermo-fluid science and engineering.

Liquid Film Cooling in Rocket Engines

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ISBN 13 :
Total Pages : 72 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Liquid Film Cooling in Rocket Engines by :

Download or read book Liquid Film Cooling in Rocket Engines written by and published by . This book was released on 1991 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt: A one-dimensional analytical model of liquid film cooling in rocket engine combustion chambers is developed and compared with existing data. The vapor generated at the liquid interface greatly decreases the convective heat flux and is treated as a 'transition' process. The radiant heat is absorbed at the walls and transmitted to the liquid film by boiling, which can lead to burnout of the film. Downstream of the liquid film, the vapor provides continued thermal protection to the wall and is treated as a gaseous film cooling process. A standard correlation is expressed in differential form to allow for the nonuniform free-stream flow in the nozzle. Liquid film lengths are well predicted by the model. Downstream of the dry-out point, wall temperatures are well predicted up to the start of convergence. Downstream of the converging turn, a correction term, correlated by a centrifugal parameter, is required to account for increased mixing at the converging turn. Downstream of the throat, wall temperatures decrease very quickly because of acceleration of the boundary- layer gases, an effect not included in the model.

Effects of Selected Gas Stream Parameters and Coolant Physical Propperties on Film Cooling of Rocket Motors

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ISBN 13 :
Total Pages : 1 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Effects of Selected Gas Stream Parameters and Coolant Physical Propperties on Film Cooling of Rocket Motors by : D. L. EMMONS

Download or read book Effects of Selected Gas Stream Parameters and Coolant Physical Propperties on Film Cooling of Rocket Motors written by D. L. EMMONS and published by . This book was released on 1962 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: The effects were studied of changes in the temperature, pressure, and Reynolds number of a hot gas stream upon the required flow rates of a single liquid (water) used for film cooling different lengths of a cylindrical test section. The effects were also studied of the physical properties of water, anhydrous ammonia, ethanol, and Freon-113 on the required film coolant flow rates for a single condition of gas stream temperature, pressure, and Reynolds number. Heat flux and wall temperature distribution downstream from the liquid film were measured. A brief investigation of combined film cooling and convective cooling was conducted. Theoretical studies also were conducted to obtain relationships for predicting the convective heat transfer coefficient between a liquid film and a flowing hot gas stream, the insulation effect provided by the film coolant vapor for areas downstream from the liquid film, and the cooling requirements when external convective cooling is supplemented with internal film cooling. The resulting equations correlated the experimental data with reasonable accuracy. (Author).

Discrete Film Cooling in a Rocket with Curved Walls

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ISBN 13 :
Total Pages : 318 pages
Book Rating : 4.:/5 (66 download)

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Book Synopsis Discrete Film Cooling in a Rocket with Curved Walls by : Jonathan Floyd McCall

Download or read book Discrete Film Cooling in a Rocket with Curved Walls written by Jonathan Floyd McCall and published by . This book was released on 2009 with total page 318 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 702 pages
Book Rating : 4.:/5 (31 download)

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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 1995 with total page 702 pages. Available in PDF, EPUB and Kindle. Book excerpt:

U.S. Government Research Reports

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ISBN 13 :
Total Pages : 1310 pages
Book Rating : 4.3/5 (243 download)

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Book Synopsis U.S. Government Research Reports by :

Download or read book U.S. Government Research Reports written by and published by . This book was released on 1964 with total page 1310 pages. Available in PDF, EPUB and Kindle. Book excerpt:

An Experimental Investigation of Gaseous -film Cooling of a Rocket Motor

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ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis An Experimental Investigation of Gaseous -film Cooling of a Rocket Motor by : James G. Lucas

Download or read book An Experimental Investigation of Gaseous -film Cooling of a Rocket Motor written by James G. Lucas and published by . This book was released on 1963 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Technical Abstract Bulletin

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ISBN 13 :
Total Pages : 98 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis Technical Abstract Bulletin by :

Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 98 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Modeling and Simulation of Mixing Layer Flows for Rocket Engine Film Cooling

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (665 download)

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Book Synopsis Modeling and Simulation of Mixing Layer Flows for Rocket Engine Film Cooling by : Kiran Hamilton Jeffrey Dellimore

Download or read book Modeling and Simulation of Mixing Layer Flows for Rocket Engine Film Cooling written by Kiran Hamilton Jeffrey Dellimore and published by . This book was released on 2010 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

U.S. Government Research Reports

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ISBN 13 :
Total Pages : 716 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis U.S. Government Research Reports by :

Download or read book U.S. Government Research Reports written by and published by . This book was released on 1964 with total page 716 pages. Available in PDF, EPUB and Kindle. Book excerpt: