Zobrazeno 1 - 10
of 53
pro vyhledávání: '"Dušan Regodić"'
Autor:
Dejan Dodić, Dušan Regodić
Publikováno v:
Tehnički Vjesnik, Vol 31, Iss 6, Pp 1995-2002 (2024)
In the current landscape of advanced natural language processing (NLP), managing GPU memory effectively is crucial. This paper delves into new tokenization methods and data handling to enhance NLP model efficiency, focusing on avoiding "CUDA out of m
Externí odkaz:
https://doaj.org/article/d8fc85d17e374d19b61d575868f06072
Autor:
Tugomir Kokelj, Dušan Regodić
Publikováno v:
Vojnotehnički Glasnik, Vol 53, Iss 2, Pp 140-156 (2005)
Postojeća metodologija za izračunavanje tačnosti potpune pripreme početnih elemenata posrednog gađanja veoma je kompleksna, nepraktična i nedovoljno tačna. U ovom radu izvršena je dorada postojeće metodologije proračuna i prikazan je adekva
Externí odkaz:
https://doaj.org/article/61a7410bfc1f40dcb84b61ae3200555d
Autor:
Dušan Regodić
Publikováno v:
Vojnotehnički Glasnik, Vol 49, Iss 3, Pp 253-266 (2001)
The automation of initial elements preparation procedure for indirect firing has been treated in this paper. Artillery firing is preceded by initial elements preparation which should be reliable as well as fast in action. Rational ammunition consumpt
Externí odkaz:
https://doaj.org/article/dac08709575f4aea91b45c9c93b53195
Autor:
Dušan Regodić
Publikováno v:
Vojnotehnički Glasnik, Vol 48, Iss 6, Pp 533-542 (2000)
Externí odkaz:
https://doaj.org/article/257ffad7a1a04c8b8438e3875abda733
Autor:
Dušan Regodić
Publikováno v:
Vojnotehnički Glasnik, Vol 48, Iss 4-5, Pp 417-424 (2000)
In the analysis of projectile flight dynamics it is of utmost importance to know the values of aerodynamic coefficients and their derivatives. The calculation of flight path elements and projectile flight stability is practically impossible without t
Externí odkaz:
https://doaj.org/article/5c59f849bde94e1b84e1982174905c16
Autor:
Dušan Regodić
Publikováno v:
Vojnotehnički Glasnik, Vol 46, Iss 5, Pp 527-538 (1998)
During a projectile flight, together with the change of angles of attack, the H, P, M and T values of Murphy's coefficients are changed depending on the change of mass characteristics and derivatives of aerodynamic coefficients in the function of the
Externí odkaz:
https://doaj.org/article/1f6d87ed825746af8c8efd34e9933e33
Autor:
Dušan Regodić
Publikováno v:
Vojnotehnički Glasnik, Vol 46, Iss 2, Pp 165-179 (1998)
The effects of dimensions and shapes of missiles on the total axial aerodynamic coefficient of resistance are presented in the paper. The calculation is done by the AERODR method and the obtained values on the diagrams are marked by CXDR. The author
Externí odkaz:
https://doaj.org/article/ac84e6e21a5b4017850142d7c29aeb3a
Autor:
Slobodan Vučković, Dušan Regodić
Publikováno v:
Vojnotehnički Glasnik, Vol 44, Iss 2, Pp 168-176 (1996)
From the exterior ballistics aspect, it is necessary to reduce projectile overall resistance during the flight in order to attain longer range. Projectile overall resistance can be reduced by optimizing its dimensions and shapes. This paper presents
Externí odkaz:
https://doaj.org/article/4487fecd1d8244e89ee95ece00396d7d
Autor:
Dušan Regodić
Publikováno v:
Vojnotehnički Glasnik, Vol 44, Iss 1, Pp 63-72 (1996)
The Pohlhausen’s method is applied to velocity profile calculation for a laminar boundary layer of a body in a streem with external velocity gradient. It is necessary to calculate boundary layer thickness, tangential stress and other parameters for
Externí odkaz:
https://doaj.org/article/35edac7b13bb467aab295eaa46cb2bc1
Autor:
Dušan Regodić
Publikováno v:
Vojnotehnički Glasnik, Vol 43, Iss 1, Pp 52-64 (1995)
Prezentiran je teorijski pristup analizi graničnog sloja pri opstrujavanju ravne i krivolinijske površine. Pored toga, dat je komparativni pristup proračunu aerodinamičkog koeficijenta otpora trenja različitih autora za laminarni, prelazni i tur
Externí odkaz:
https://doaj.org/article/c14ebb925316413fa249fcacba61fd93