MILINOVIC, Momcilo Pane;JERKOVIĆ, Damir Drago;JEREMIĆ, Olivera M;KOVAČ, Mitar . Experimental and Simulation Testing of Flight Spin Stability for Small Caliber Cannon Projectile. Strojniški vestnik - Journal of Mechanical Engineering, [S.l.], v. 58, n.6, p. 394-402, june 2018. ISSN 0039-2480. Available at: <https://www.sv-jme.eu/article/experimental-and-simulation-testing-of-flight-spin-stability-for-small-caliber-cannon-projectile/>. Date accessed: 22 dec. 2024. doi:http://dx.doi.org/10.5545/sv-jme.2011.277.
Milinovic, M., Jerković, D., Jeremić, O., & Kovač, M. (2012). Experimental and Simulation Testing of Flight Spin Stability for Small Caliber Cannon Projectile. Strojniški vestnik - Journal of Mechanical Engineering, 58(6), 394-402. doi:http://dx.doi.org/10.5545/sv-jme.2011.277
@article{sv-jmesv-jme.2011.277,
author = {Momcilo Pane Milinovic and Damir Drago Jerković and Olivera M Jeremić and Mitar Kovač},
title = {Experimental and Simulation Testing of Flight Spin Stability for Small Caliber Cannon Projectile},
journal = {Strojniški vestnik - Journal of Mechanical Engineering},
volume = {58},
number = {6},
year = {2012},
keywords = {aerodynamic coefficients spin stabilized small caliber cannon projectile; gyroscopic stability factor; dynamic stability factor; damping stability coefficients},
abstract = {The basic aim of this paper is to consider correlations of stability flight criteria, derived as the relations of aerodynamic coefficients and derivatives, on the model of small caliber cannon spin stabilized projectile. Model of stability criteria calculations are performed by experimentally testing of aerodynamic data in the wind tunnel, and composed with the semi-empirical data, both applied on the flight trajectory stability simulation test. Authors’ wind tunnel tests and calculated values of aerodynamic coefficients, as function of Mach numbers of projectile model are presented in the simulation flight trajectories stability criteria. The comparative analysis of experimental and calculated aerodynamic coefficients of projectile model is done, refers to the stability flight criteria. Calculation of projectile aerodynamic Magnus moment derivatives, with other aerodynamic representatives, is used as the critical stability factors testing data vs. flight Mach numbers. Influences of this derivative absence and presence on the model sequence of the flight trajectory are presented for the estimation of angles of attack damping and stability factors. Simulation tests are presented for the supersonic and subsonic integral flight velocities and spin damping data. Research is realized due to the considerations of further projectiles correction possibilities on trajectory, and other new applications, vs. existing of unreliable lateral moments.},
issn = {0039-2480}, pages = {394-402}, doi = {10.5545/sv-jme.2011.277},
url = {https://www.sv-jme.eu/article/experimental-and-simulation-testing-of-flight-spin-stability-for-small-caliber-cannon-projectile/}
}
Milinovic, M.,Jerković, D.,Jeremić, O.,Kovač, M. 2012 June 58. Experimental and Simulation Testing of Flight Spin Stability for Small Caliber Cannon Projectile. Strojniški vestnik - Journal of Mechanical Engineering. [Online] 58:6
%A Milinovic, Momcilo Pane %A Jerković, Damir Drago %A Jeremić, Olivera M %A Kovač, Mitar %D 2012 %T Experimental and Simulation Testing of Flight Spin Stability for Small Caliber Cannon Projectile %B 2012 %9 aerodynamic coefficients spin stabilized small caliber cannon projectile; gyroscopic stability factor; dynamic stability factor; damping stability coefficients %! Experimental and Simulation Testing of Flight Spin Stability for Small Caliber Cannon Projectile %K aerodynamic coefficients spin stabilized small caliber cannon projectile; gyroscopic stability factor; dynamic stability factor; damping stability coefficients %X The basic aim of this paper is to consider correlations of stability flight criteria, derived as the relations of aerodynamic coefficients and derivatives, on the model of small caliber cannon spin stabilized projectile. Model of stability criteria calculations are performed by experimentally testing of aerodynamic data in the wind tunnel, and composed with the semi-empirical data, both applied on the flight trajectory stability simulation test. Authors’ wind tunnel tests and calculated values of aerodynamic coefficients, as function of Mach numbers of projectile model are presented in the simulation flight trajectories stability criteria. The comparative analysis of experimental and calculated aerodynamic coefficients of projectile model is done, refers to the stability flight criteria. Calculation of projectile aerodynamic Magnus moment derivatives, with other aerodynamic representatives, is used as the critical stability factors testing data vs. flight Mach numbers. Influences of this derivative absence and presence on the model sequence of the flight trajectory are presented for the estimation of angles of attack damping and stability factors. Simulation tests are presented for the supersonic and subsonic integral flight velocities and spin damping data. Research is realized due to the considerations of further projectiles correction possibilities on trajectory, and other new applications, vs. existing of unreliable lateral moments. %U https://www.sv-jme.eu/article/experimental-and-simulation-testing-of-flight-spin-stability-for-small-caliber-cannon-projectile/ %0 Journal Article %R 10.5545/sv-jme.2011.277 %& 394 %P 9 %J Strojniški vestnik - Journal of Mechanical Engineering %V 58 %N 6 %@ 0039-2480 %8 2018-06-28 %7 2018-06-28
Milinovic, Momcilo, Damir Drago Jerković, Olivera M Jeremić, & Mitar Kovač. "Experimental and Simulation Testing of Flight Spin Stability for Small Caliber Cannon Projectile." Strojniški vestnik - Journal of Mechanical Engineering [Online], 58.6 (2012): 394-402. Web. 22 Dec. 2024
TY - JOUR AU - Milinovic, Momcilo Pane AU - Jerković, Damir Drago AU - Jeremić, Olivera M AU - Kovač, Mitar PY - 2012 TI - Experimental and Simulation Testing of Flight Spin Stability for Small Caliber Cannon Projectile JF - Strojniški vestnik - Journal of Mechanical Engineering DO - 10.5545/sv-jme.2011.277 KW - aerodynamic coefficients spin stabilized small caliber cannon projectile; gyroscopic stability factor; dynamic stability factor; damping stability coefficients N2 - The basic aim of this paper is to consider correlations of stability flight criteria, derived as the relations of aerodynamic coefficients and derivatives, on the model of small caliber cannon spin stabilized projectile. Model of stability criteria calculations are performed by experimentally testing of aerodynamic data in the wind tunnel, and composed with the semi-empirical data, both applied on the flight trajectory stability simulation test. Authors’ wind tunnel tests and calculated values of aerodynamic coefficients, as function of Mach numbers of projectile model are presented in the simulation flight trajectories stability criteria. The comparative analysis of experimental and calculated aerodynamic coefficients of projectile model is done, refers to the stability flight criteria. Calculation of projectile aerodynamic Magnus moment derivatives, with other aerodynamic representatives, is used as the critical stability factors testing data vs. flight Mach numbers. Influences of this derivative absence and presence on the model sequence of the flight trajectory are presented for the estimation of angles of attack damping and stability factors. Simulation tests are presented for the supersonic and subsonic integral flight velocities and spin damping data. Research is realized due to the considerations of further projectiles correction possibilities on trajectory, and other new applications, vs. existing of unreliable lateral moments. UR - https://www.sv-jme.eu/article/experimental-and-simulation-testing-of-flight-spin-stability-for-small-caliber-cannon-projectile/
@article{{sv-jme}{sv-jme.2011.277},
author = {Milinovic, M., Jerković, D., Jeremić, O., Kovač, M.},
title = {Experimental and Simulation Testing of Flight Spin Stability for Small Caliber Cannon Projectile},
journal = {Strojniški vestnik - Journal of Mechanical Engineering},
volume = {58},
number = {6},
year = {2012},
doi = {10.5545/sv-jme.2011.277},
url = {https://www.sv-jme.eu/article/experimental-and-simulation-testing-of-flight-spin-stability-for-small-caliber-cannon-projectile/}
}
TY - JOUR AU - Milinovic, Momcilo Pane AU - Jerković, Damir Drago AU - Jeremić, Olivera M AU - Kovač, Mitar PY - 2018/06/28 TI - Experimental and Simulation Testing of Flight Spin Stability for Small Caliber Cannon Projectile JF - Strojniški vestnik - Journal of Mechanical Engineering; Vol 58, No 6 (2012): Strojniški vestnik - Journal of Mechanical Engineering DO - 10.5545/sv-jme.2011.277 KW - aerodynamic coefficients spin stabilized small caliber cannon projectile, gyroscopic stability factor, dynamic stability factor, damping stability coefficients N2 - The basic aim of this paper is to consider correlations of stability flight criteria, derived as the relations of aerodynamic coefficients and derivatives, on the model of small caliber cannon spin stabilized projectile. Model of stability criteria calculations are performed by experimentally testing of aerodynamic data in the wind tunnel, and composed with the semi-empirical data, both applied on the flight trajectory stability simulation test. Authors’ wind tunnel tests and calculated values of aerodynamic coefficients, as function of Mach numbers of projectile model are presented in the simulation flight trajectories stability criteria. The comparative analysis of experimental and calculated aerodynamic coefficients of projectile model is done, refers to the stability flight criteria. Calculation of projectile aerodynamic Magnus moment derivatives, with other aerodynamic representatives, is used as the critical stability factors testing data vs. flight Mach numbers. Influences of this derivative absence and presence on the model sequence of the flight trajectory are presented for the estimation of angles of attack damping and stability factors. Simulation tests are presented for the supersonic and subsonic integral flight velocities and spin damping data. Research is realized due to the considerations of further projectiles correction possibilities on trajectory, and other new applications, vs. existing of unreliable lateral moments. UR - https://www.sv-jme.eu/article/experimental-and-simulation-testing-of-flight-spin-stability-for-small-caliber-cannon-projectile/
Milinovic, Momcilo, Jerković, Damir, Jeremić, Olivera, AND Kovač, Mitar. "Experimental and Simulation Testing of Flight Spin Stability for Small Caliber Cannon Projectile" Strojniški vestnik - Journal of Mechanical Engineering [Online], Volume 58 Number 6 (28 June 2018)
Strojniški vestnik - Journal of Mechanical Engineering 58(2012)6, 394-402
© The Authors, CC-BY 4.0 Int. Change in copyright policy from 2022, Jan 1st.
The basic aim of this paper is to consider correlations of stability flight criteria, derived as the relations of aerodynamic coefficients and derivatives, on the model of small caliber cannon spin stabilized projectile. Model of stability criteria calculations are performed by experimentally testing of aerodynamic data in the wind tunnel, and composed with the semi-empirical data, both applied on the flight trajectory stability simulation test. Authors’ wind tunnel tests and calculated values of aerodynamic coefficients, as function of Mach numbers of projectile model are presented in the simulation flight trajectories stability criteria. The comparative analysis of experimental and calculated aerodynamic coefficients of projectile model is done, refers to the stability flight criteria. Calculation of projectile aerodynamic Magnus moment derivatives, with other aerodynamic representatives, is used as the critical stability factors testing data vs. flight Mach numbers. Influences of this derivative absence and presence on the model sequence of the flight trajectory are presented for the estimation of angles of attack damping and stability factors. Simulation tests are presented for the supersonic and subsonic integral flight velocities and spin damping data. Research is realized due to the considerations of further projectiles correction possibilities on trajectory, and other new applications, vs. existing of unreliable lateral moments.