This paper presents small scale reverse ballistic experiments and hydrocode simulations to estimate the influence of aerodynamic heating on the terminal ballistic performance of a hypervelocity kinetic energy projectile. A 3mm diameter, L/D 10 tungsten alloy projectile was heated to temperatures up
โฆ LIBER โฆ
Aerodynamic heating of ballistic missile including the effects of gravity
โ Scribed by S. N. Maitra
- Book ID
- 110637732
- Publisher
- Indian Academy of Sciences
- Year
- 2000
- Tongue
- English
- Weight
- 96 KB
- Volume
- 25
- Category
- Article
- ISSN
- 0256-2499
No coin nor oath required. For personal study only.
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