Liquid Rocket Engine Combustion (12 results)
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Seller: preigu, Osnabrück, Germanypreigu
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Taschenbuch. Condition: Neu. High Frequency Combustion Instabilities in the DVRC Rocket Combustor | Experimental Study of Combustion Instabilities in a Liquid Rocket Engine | Andrea Terracciano | Taschenbuch | 204 S. | Englisch | 2015 | LAP LAMBERT Academic Publishing | EAN 9783659639166 | Verantwortliche Person für die EU: BoD…- Books on Demand, In de Tarpen 42, 22848 Norderstedt, info[at]bod[dot]de | Anbieter: preigu.
Language: English
Published by American Institute of Aeronautics & Astronautics, 1995
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Seller: Revaluation Books, Exeter, United KingdomRevaluation Books
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US$ 169.69
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Hardcover. Condition: Brand New. 577 pages. 9.25x6.25x1.25 inches. In Stock.
Liquid Rocket Engine Combustion Instruction (Progress in Astronautics and Aeronautics)
Yang, Yang, Professor Vigor, V Yang and W Anderson, Pennsylv
Language: English
Published by AIAA (American Institute of Aeronautics & Astronau, 1995
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Seller: Mispah books, Redhill, SURRE, United KingdomMispah books
Contact seller4-star sellerCondition: New
US$ 275.77
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Hardcover. Condition: New. NEW. SHIPS FROM MULTIPLE LOCATIONS. book.
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Language: English
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Seller: S N Books World, Delhi, IndiaS N Books World
Contact seller5-star sellerLeatherbound. Condition: NEW. BOOKS ARE EXEMPT FROM IMPORT DUTIES AND TARIFFS; NO EXTRA CHARGES APPLY. Leather Binding on Spine and Corners with Golden leaf printing on spine. Bound in genuine leather with Satin ribbon page markers and Spine with raised gilt bands. A perfect gift for your loved ones. Reprinted from 1961 edition.… NO changes have been made to the original text. This is NOT a retyped or an ocr'd reprint. Illustrations, Index, if any, are included in black and white. Each page is checked manually before printing. As this print on demand book is reprinted from a very old book, there could be some missing or flawed pages, but we always try to make the book as complete as possible. Fold-outs, if any, are not part of the book. If the original book was published in multiple volumes then this reprint is of only one volume, not the whole set and contains approximately 28 pages. IF YOU WISH TO ORDER PARTICULAR VOLUME OR ALL THE VOLUMES YOU CAN CONTACT US. Resized as per current standards. Sewing binding for longer life, where the book block is actually sewn (smythe sewn/section sewn) with thread before binding which results in a more durable type of binding. Language: English.
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Seller: liu xing, Nanjing, JS, Chinaliu xing
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US$ 62.50
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paperback. Condition: New. Language:Chinese.Pages Number: 202 Publisher: Defense Industry Pub. Date :2011-04-01 version 1. liquid rocket engine combustion kinetics of liquid rocket engine development and design process. an important element. Nie Wansheng edited the liquid rocket engine combustion kinetics model and numerical cal…culation. a systematic introduction to liquid rocket engine combustion kinetics model and numerical method. numerical calculations are discussed in the hypergolic propellant. propellant and cryo.
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Seller: liu xing, Nanjing, JS, Chinaliu xing
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US$ 86.32
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Hardcover. Condition: New. HardCover. Pub Date :2012-06-01 Publisher: National Defense Industry Press Only genuine brand new book No pictures. Baidu. check the title ISBN pricing Publishing House; only puerile - can not counter-offer. Could not free open textbook amount of the invoice is not taxed. books dedicated machine-printe…d invoices.
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Seller: liu xing, Nanjing, JS, Chinaliu xing
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US$ 87.83
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paperback. Condition: New. Ship out in 2 business day, And Fast shipping, Free Tracking number will be provided after the shipment.Paperback. Pub Date :2001-02-01 Pages: 466 Language: Chinese Publisher: Science Press copy printing is clear. such as the original book . not the kind of dao version of the book . paper. copy paper i…s very thick kind of paper . before making contact and then shipped . thank you ! Title: liquid rocket engine combustion instability Author: (U.S. ) v Young ( America ) we Anderson Publisher : Science Press Price: 60.0 Basic information : Publication Date :2001 -02 Packaging: Paperback Folio: 16 P.Four Satisfaction guaranteed,or money back.
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Seller: liu xing, Nanjing, JS, Chinaliu xing
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paperback. Condition: New. Ship out in 2 business day, And Fast shipping, Free Tracking number will be provided after the shipment.Pub Date :2012-10-01 Pages: 280 Publisher: National Defense Industry Press liquid rocket engine combustion process modeling and numerical simulation. systematically establish and introduce a spray of… liquid rocket engine combustion process theories. models and numerical methods . including liquid propellant spray nozzle atomization theories and models droplets at atmospheric pressure . pressure and vibration environments and multi-component droplet evaporation theory evaporation model . turbu.Four Satisfaction guaranteed,or money back.
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Language: English
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Seller: S N Books World, Delhi, IndiaS N Books World
Contact seller5-star sellerLeatherBound. Condition: New. BOOKS ARE EXEMPT FROM IMPORT DUTIES AND TARIFFS; NO EXTRA CHARGES APPLY. Leatherbound edition. Condition: New. Leather Binding on Spine and Corners with Golden leaf printing on spine. Bound in genuine leather with Satin ribbon page markers and Spine with raised gilt bands. Pages: 136. A perfect gift… for your loved ones. Reprinted from 1975 edition. NO changes have been made to the original text. This is NOT a retyped or an ocr'd reprint. Illustrations, Index, if any, are included in black and white. Each page is checked manually before printing. As this print on demand book is reprinted from a very old book, there could be some missing or flawed pages, but we always try to make the book as complete as possible. Fold-outs, if any, are not part of the book. If the original book was published in multiple volumes then this reprint is of only one volume, not the whole set. IF YOU WISH TO ORDER PARTICULAR VOLUME OR ALL THE VOLUMES YOU CAN CONTACT US. Resized as per current standards. Sewing binding for longer life, where the book block is actually sewn (smythe sewn/section sewn) with thread before binding which results in a more durable type of binding. Language: English Pages: 136.
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Seller: True World of Books, Delhi, IndiaTrue World of Books
Contact seller5-star sellerLeatherBound. Condition: New. BOOKS ARE EXEMPT FROM IMPORT DUTIES AND TARIFFS; NO EXTRA CHARGES APPLY. LeatherBound edition. Condition: New. Reprinted from 1967 edition. Leather Binding on Spine and Corners with Golden leaf printing on spine. Bound in genuine leather with Satin ribbon page markers and Spine with raised gilt band…s. A perfect gift for your loved ones. Pages: 152 NO changes have been made to the original text. This is NOT a retyped or an ocr'd reprint. Illustrations, Index, if any, are included in black and white. Each page is checked manually before printing. As this print on demand book is reprinted from a very old book, there could be some missing or flawed pages, but we always try to make the book as complete as possible. Fold-outs, if any, are not part of the book. If the original book was published in multiple volumes then this reprint is of only one volume, not the whole set. Sewing binding for longer life, where the book block is actually sewn (smythe sewn/section sewn) with thread before binding which results in a more durable type of binding. Pages: 152 Kelly, Robert Joseph.
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Seller: liu xing, Nanjing, JS, Chinaliu xing
Contact seller5-star sellerCondition: New
US$ 399.83
US$ 18.00 shippingShips from China to U.S.A.Quantity: 3 available
Hardcover. Condition: New. HardCover. Pub Date: 2016-07-01 Pages: 382 Language: English Publisher: national defense industry press the liquid rocket engine combustion process modeling and numerical simulation (English version) is the author zhen-guo wang engaged in liquid rocket engine combustion process numerical summary of the… research. and reflect the status of current research and development at home and abroad.The book has.
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Seller: AHA-BUCH GmbH, Einbeck, GermanyAHA-BUCH GmbH
Contact seller5-star sellerCondition: New
US$ 84.25
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Taschenbuch. Condition: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - This experimental work regards the studies of the high frequency combustion instabilities inside the DVRC (Discretely Variable Resonance Combustor), a liquid rocket engine, developed by the Purdue University at M. J. Zucrow Laboratories,… on behalf of Nasa Marshall Space Flight Center. The research revealed that, given these specific flow conditions, combustion instability occurs inside the system during hot fire tests. The most important experimental result of the study showed the oxidizer manifold acting as a damper of the pressure oscillations coming from the combustion chamber and how this can represent an advantage in terms of reduced mechanical loads at the interface with the rest of the feed system. The LEE code based on the linearized Euler equations detected both the combustion instability inside the DVRC and confirmed the positive role of the oxidizer manifold. The best agreement with the experimental results has been observed considering heat addition at the plane of propellants injection into the combustion chamber, showing it is reasonable to assume combustion occurs mainly in proximity of that plane, as the previous works about CVRC and CFD results had already shown.
