[4] Bonner E., Clever W. and Dunn K. Aerodynamic Preliminary Analysis System II:
Part I Theory. NASA-CR-165627, Apr. 1981. 127 p.
[5] Smyth D.N. and Loo H.C. Analysis of Static Pressure Data from 1/12-scale Model
of the YF-12A. Vol. 3: The MARK IVS Supersonic-Hypersonic Arbitrary Body
Program. User’s Manual, 1981, NASA-CR-151940.
[6] Cunningham M. Hypersonic Aerodynamics for an Entry Research Vehicle.
J.
Spacecraft and Rockets
. 1987, vol. 24, no. 2, pp. 97–98.
[7] Kinney D.J. Aero-Thermodynamics for Conceptual Design.
42nd AIAA Aerospace
Sciences Meeting and Exhibit
, Reno, NV, 5–8 Jan. 2004, AIAA-2004-31-
962. Available at:
-
31-871.pdf (accessed 02.11.13).
[8] Barnes J., Hut P. A hierarchical O (N log N) force-calculation algorithm.
Nature
, 324
(4), 1986, pp. 446–449.
[9] Asmolovskiy N.A., Baskakov V.D., Tarasov V.A. Influence analysis of periodical
perturbations on the formation of high-speed rod element.
Izv. Vyssh. Uchebn. Zaved.,
Mashinostr.
[Proc. Univ., Mech. Eng.], 2013, no. 8, pp. 8–14 (in Russ.).
[10] Scott R.D. Ray Casting for Modeling Solids.
Computer Graphics and Image
Processing
, 1982, vol. 18, no. 2, pp. 109–144.
[11] Mark de Berg. Ray Shooting, Depth Orders and Hidden Surface Removal. Springer,
1993. 210 p.
[12] Kolpakov V.I., Baskakov V.D., Kruzhkov O.A., Shikunov N.V. Impact evaluation
of technological factors on kinematic parameters of the elongated damage agent
for shaped charge. Tr. Mezhdunar. Konf. IX Kharitonovskie tematicheskie nauchnye
chteniya: Ekstremal’nye sostoyaniya veshchestva. Detonatsiya. Udarnye volny [Proc.
Int. Conf. IX Kharitonov Topical Scientific Readings: Extreme states of matter.
Detonation. Shock waves], 2007, pp. 585–590 (in Russ.).
[13] Bender D., Chhouk B., Fong R., Ng W., Rice B., Volkmann E. Explosively formed
penetrators with canted fins.
Proc. 19th Int. Symp. Ballistics.
, 2001, pp. 755–762.
[14] Hoffman J., Frankel S. Numerical Methods for Engineers and Scientists. CRC Press,
2001. 840 p.
[15] Mathematical maintenance of probabilistic estimation influence of technological
errors on efficiency of elongated strike elements of the shells forming explosive
charges.
Oboronnaya tekhnika
[Defence Technology], 2009, vol. 1, no. 1, pp. 49–53
(in Russ.).
Статья поступила в редакцию 17.03.2014
Асмоловский Николай Александрович — аспирант кафедры “Технологии ракетно-
космического машиностроения” МГТУ им. Н.Э. Баумана. Автор пяти научных работ
в области технологии ракетно-космического машиностроения.
МГТУ им. Н.Э. Баумана, Российская Федерация, 105005, Москва, 2-я Бауманская ул.,
д. 5.
N.A. Asmolovskiy — post-graduate of “Technologies of Rocket and Space Mechanical
Engineering” department of the Bauman Moscow State Technical University. Author of
five publications in the field of technology of rocket and space mechanical engineering.
Bauman Moscow State Technical University, Vtoraya Baumanskaya ul. 5, Moscow,
105005 Russian Federation.
Баскаков Владимир Дмитриевич — д-р техн. наук, профессор кафедры “Технологии
ракетно-космического машиностроения” МГТУ им. Н.Э. Баумана. Автор 90 научных
работ в области технологии ракетно-космического машиностроения.
МГТУ им. Н.Э. Баумана, Российская Федерация, 105005, Москва, 2-я Бауманская ул.,
д. 5.
ISSN 0236-3941. Вестник МГТУ им. Н.Э. Баумана. Сер. “Машиностроение” 2014. № 4 121