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Unsteady Effects of Shock-Induced Separation(Chinese Edition)
Da: liu xing, Nanjing, JS, Cina
Valutazione del venditore 5 su 5 stelle
Hardcover. Condizione: New. HardCover. Pub Date: 2022-10-01 Pages: 288 Language: Chinese Publisher: Science Press Unsteady Effects of Shock-Induced Separation focuses on three basic configurations of transonic airfoil. nozzle flow. and oblique shock wave reflection Introduce the research progress of the unsteady problem of shock wave/boundary layer interference. give a large number of unsteady pressure and aerodynamic experimental data. and compare with the results of different numerical simulation methods. and evaluate. Codice articolo NY043577
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