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Aircraft & Rocket Turbines - Physics and Design

Autor A. H. Epstein Editat de J. Vennard
en Limba Engleză Paperback – 30 apr 2008
Section titles are ...(1) Introduction ...(2) Compressor Flutter Clearance Methodology ...(3) Physics of Coolants and Main Flow Interactions in Aircraft and Rocket Turbines ...(4) Role of Tip Clearance Flow on Axial Compressor Stability ...(6) Impact of Tip Clearance Flow on Centrifugal Impeller Pump Performance ...(7) Fabrication and Testing of Compressor Rotor Blades ...(8) Appendix.
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Specificații

ISBN-13: 9781934939185
ISBN-10: 1934939188
Pagini: 156
Dimensiuni: 210 x 279 x 8 mm
Greutate: 0.37 kg
Editura: Wexford College Press

Descriere

This resource about the advances in physics and design as applied to aircraft and rocket turbines covers compressor flutter clearance methodology, the physics of coolants, the role and impact of tip clearance flow, and fabrication and testing. (Technology & Industrial Arts)