Autor: Zygmunt, K. - Katalog OPAC zbiorów

Skocz do pozycji: 1.

Tytuł:: Theoretical and experimental research of anti-tank kinetic penetrator ballistics
Autorzy:: Motyl, K.
Magier, M.
Borkowski, J.
Zygmunt, B.
Powiązania:: https://bibliotekanauki.pl/articles/200983.pdf
Data publikacji:: 2017
Wydawca:: Polska Akademia Nauk. Czytelnia Czasopism PAN
Tematy:: hypersonic projectile
mathematical model
simulation of flight
pocisk militarny
model matematyczny
Symulacja lotu
Opis:: A mathematical-physical model of the hypersonic anti-tank kinetic subcalibre projectile for 120 mm munition was built. Computer simulations of the projectile flight were performed for any angle of shooting, from 0° to 90°. Trajectories of projectile flights were determined considering all angles of shooting. Theoretical calculations were verified by experimental measurement of the projectile velocity in time while shooting on a test range. Some conclusions with regard to safety during hypersonic projectile shooting on the test range were formulated.
Źródło:: Bulletin of the Polish Academy of Sciences. Technical Sciences; 2017, 65, 3; 399-404
0239-7528
Pojawia się w:: Bulletin of the Polish Academy of Sciences. Technical Sciences
Dostawca treści:: Biblioteka Nauki

Artykuł

Skocz do pozycji: 2.

Tytuł:: Theoretical and experimental research of supersonic missile ballistics
Autorzy:: Zygmunt, B.
Motyl, K.
Machowski, B.
Makowski, M.
Olejniczak, E.
Powiązania:: https://bibliotekanauki.pl/articles/201046.pdf
Data publikacji:: 2015
Wydawca:: Polska Akademia Nauk. Czytelnia Czasopism PAN
Tematy:: missile exterior ballistics
mathematical model
computer simulation
test range experiment
pociski balistyczne
model matematyczny
symulacja komputerowa
Opis:: A mathematical-physical model of a supersonic missile was built, taking into account the mass and inertia properties. The model was implemented in the MathCAD14 simulation program. A numerical analysis of the missile ballistics was conducted and basic parameters were determined: range, altitude, velocity and acceleration, which enabled a test range program for manufactured missile models to be drawn up. Initial flight tests of missiles were carried out at the test range. Satisfactory accordance of experimental and theoretical dynamic parameters of the missile under study was obtained.
Źródło:: Bulletin of the Polish Academy of Sciences. Technical Sciences; 2015, 63, 1; 229-233
0239-7528
Pojawia się w:: Bulletin of the Polish Academy of Sciences. Technical Sciences
Dostawca treści:: Biblioteka Nauki

Artykuł

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