A special design condition to increase the performance of two-stage light-gas guns

被引:24
作者
Francesconi, A. [1 ]
Pavarin, D. [1 ]
Bettella, A. [1 ]
Angrilli, F. [1 ]
机构
[1] Univ Padua, CISAS G Colombo, I-35131 Padua, Italy
关键词
Two-stage light-gas gun; Optimization; Sizing; Base pressure;
D O I
10.1016/j.ijimpeng.2008.07.035
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
This paper reports a theoretical and numerical study aimed at increasing the operating efficiency of two-stage light-gas guns by appropriately changing their working conditions. In particular, a method is presented for increasing the projectile speed without any rise of the maximum breech pressure. The classic design theory of two-stage guns starts from the assumption that the highest velocity is reached in a gun which constantly maintains the maximum acceptable pressure at the base of the projectile during the full launching time. The main drawback of this working condition is that it may require an unfeasible rise of the gun maximum pressure, especially when very high muzzle speed is requested. To overcome this limitation, a new reference case different from the constant-base-pressure one is presented, based on a novel gas-dynamics solution that can be expressed in exact form if losses are not accounted for. According to such an approach, it is theoretically shown that the projectile base-pressure can be appropriately shaped (i) to improve the final speed without increasing the breech pressure or, in other terms, (ii) to achieve a given muzzle velocity with reduced maximum gas pressure. The analytical application of the new gas-dynamics condition showed the capability of obtaining a 1 km/s velocity improvement with no increase of the breech pressure or, alternatively, a pressure reduction up to 30% with no penalty on the model final speed. A numerical verification of the calculations was performed through the CISAS light-gas gun full numerical model, which includes real effects such as friction losses and heat transfer. Finally, an experimental verification of the numerical test case was attempted and a speed augmentation of 0.8 km/s with no increase in the breech pressure was confirmed in laboratory, highlighting the agreement with numerical predictions. (C) 2008 Elsevier Ltd. All rights reserved.
引用
收藏
页码:1510 / 1515
页数:6
相关论文
共 13 条
[1]  
Angrilli F, 2003, ACTA ASTRONAUT, V53, P185
[2]  
CANNING TN, 1970, BALLISTIC RANGE TECH, P138
[3]   Enhanced hypervelocity launcher - Capabilities to 16 km/s [J].
Chhabildas, LC ;
Kmetyk, LN ;
Reinhart, WD ;
Hall, CA .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 1995, 17 (1-3) :183-194
[4]   AN IMPACT TECHNIQUE TO ACCELERATE FLIER PLATES TO VELOCITIES OVER 12 KM/S [J].
CHHABILDAS, LC ;
DUNN, JE ;
REINHART, WD ;
MILLER, JM .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 1993, 14 (1-4) :121-132
[5]  
FRANCESCONI A, 2001, P 16 C NAZ AIDAA
[6]   A HYPERVELOCITY - MICROPARTICLE - IMPACTS LABORATORY WITH 100-KM S PROJECTILES [J].
KEATON, PW ;
IDZOREK, GC ;
ROWTON, LJ ;
SEAGRAVE, JD ;
STRADLING, GL ;
BERGESON, SD ;
COLLOPY, MT ;
CURLING, HL ;
MCCOLL, DB ;
SMITH, JD .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 1990, 10 (1-4) :295-308
[7]   Improvement of the CISAS high-shot-frequency light-gas gun [J].
Pavarin, D ;
Francesconi, A .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 2003, 29 (1-10) :549-562
[8]  
PAVARIN D, 2004, P 55 ARA M
[9]  
PAVARIN D, 052002 CISAS
[10]  
SCHWARTZ AJ, 1999, P 18 S BALL