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Thermofluiddynamics of Optimized Rocket Propulsions
Daniel Straub
€ 54.99
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Description for Thermofluiddynamics of Optimized Rocket Propulsions
Paperback. Num Pages: 266 pages, biography. BIC Classification: PHDF; TGB; TRP. Category: (P) Professional & Vocational. Dimension: 229 x 152 x 14. Weight in Grams: 402.
This study has two declared aims: it presents the theoretical basis for a provably ideal comparative process for relaxing flows (ICP) and jus tifies its application to jet and, in particular, rocket engines. This will be treated in two parts. Part I offers a status quo report on current calculation methods, and compiles and explains briefly the most important data on selected pro minent rocket engines. Starting from the phenomenology of the dynamical and physico-chemical conversion processes in the fuel-oxidizer fluid mixture and in the burned gases, the ideal thermodynamic comparative process is then derived - as a defined sequential ... Read more
This study has two declared aims: it presents the theoretical basis for a provably ideal comparative process for relaxing flows (ICP) and jus tifies its application to jet and, in particular, rocket engines. This will be treated in two parts. Part I offers a status quo report on current calculation methods, and compiles and explains briefly the most important data on selected pro minent rocket engines. Starting from the phenomenology of the dynamical and physico-chemical conversion processes in the fuel-oxidizer fluid mixture and in the burned gases, the ideal thermodynamic comparative process is then derived - as a defined sequential ... Read more
Product Details
Format
Paperback
Publication date
2011
Publisher
Springer Basel Switzerland
Number of pages
266
Condition
New
Number of Pages
266
Place of Publication
Basel, Switzerland
ISBN
9783034899277
SKU
V9783034899277
Shipping Time
Usually ships in 15 to 20 working days
Ref
99-15
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