"Introducing the state-of-the-art of hypervelocity shock tunnels, this complete reference features a variety of drivers and step-by-step introductions to their theories, physics, methods and testing. This book enables researchers and engineers in aerospace to design and improve wind tunnels that simulate flow qualities of real hypersonic flyers"--
"Introducing the state-of-the-art of hypervelocity shock tunnels, this complete reference features a variety of drivers and step-by-step introductions to their theories, physics, methods and testing. This book enables researchers and engineers in aerospace to design and improve wind tunnels that simulate flow qualities of real hypersonic flyers"--Hinweis: Dieser Artikel kann nur an eine deutsche Lieferadresse ausgeliefert werden.
Zonglin Jiang is a professor of the Institute of Mechanics, Chinese Academy of Sciences (CAS), a Distinguished Fellow of the International Shock Wave Institute (ISWI), a Member of Russian Academy of Natural Sciences and an AIAA Associate Fellow. He has been internationally recognized for his universal framework of detonation initiation and propagation, the theory and technology for detonation-driven hypervelocity shock tunnels, the standing oblique detonation ramjet engine and the dispersion-controlled dissipative shock-capturing scheme, and rewarded the 2016 AIAA Ground Testing Award, the National Technology Invention Prize of China, the Outstanding Scientific and Technology Achievement Prize of CAS.
Inhaltsangabe
1. Introduction; 2. Shock wave relations and aerothermodynamic states; 3. Heated light gas high enthalpy shock tunnels; 4. Free piston driven high enthalpy shock tunnels; 5. Detonation driven high enthalpy shock tunnels; 6. Theory and methods for long test duration shock tunnels; 7. Methods for designing high enthalpy flow nozzles; 8. Aero thermal dynamic testing and hypersonic physics.
1. Introduction; 2. Shock wave relations and aerothermodynamic states; 3. Heated light gas high enthalpy shock tunnels; 4. Free piston driven high enthalpy shock tunnels; 5. Detonation driven high enthalpy shock tunnels; 6. Theory and methods for long test duration shock tunnels; 7. Methods for designing high enthalpy flow nozzles; 8. Aero thermal dynamic testing and hypersonic physics.
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