Seller: liu xing, Nanjing, JS, China
paperback. Condition: New. Paperback. Pub Date: 2015-12-01 Pages: 244 Language: Chinese Publisher: National Defense Industry Press field rocket engine numerical methods to assess the structural integrity is based on the theory of viscoelastic. viscoelastic incremental finite element numerical method to calculate adherent casting type field and free loading rocket engine response under various loads of history. to assess the structural integrity of the engine. and the use of visco elastic fracture finite element analysi.