Librería: liu xing, Nanjing, JS, China
Hardcover. Condición: 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. Nº de ref. del artículo: NY043577
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