Geodesic
К~задаче математического моделирования гиперзвуковой космической крылатой ракеты
Journal of Samara State Technical University, Ser. Physical and Mathematical Sciences, Journal of Samara State Technical University, Ser. Physical and Mathematical Sciences, no. 38 (2005), pp. 142-147.

Voir la notice de l'article provenant de la source Math-Net.Ru

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O. V. Kolgotin; L. V. Kudyurov. К~задаче математического моделирования гиперзвуковой космической крылатой ракеты. Journal of Samara State Technical University, Ser. Physical and Mathematical Sciences, Journal of Samara State Technical University, Ser. Physical and Mathematical Sciences, no. 38 (2005), pp. 142-147. http://geodesic.mathdoc.fr/item/VSGTU_2005_38_a24/

[1] Kolgotin O. V., “Issledovanie reaktivnogo dvizheniya dlya sozdaniya novykh klassov reaktivnykh dvigatelei”, Sb. nauchnykh trudov universit. seminara po sistemnomu analizu upravleniya i obrabotke informatsii, Penz. gos. un-t, Penza, 2001, 7

[2] Feodosev V. I., Osnovy tekhniki raketnogo poleta, Nauka, M., 1979

[3] Kolgotin O. V., Mekhanicheskaya model dvizheniya tela peremennoi massy v srede, Penzenskii tsentr nauchno-tekhnicheskoi informatsii, Penza, 2000

[4] Kurziner R. I., Reaktivnye dvigateli dlya bolshikh sverkhzvukovykh skorostei poleta, Mashinostroenie, M., 1989