A method to define low-altitude rocket exhaust characteristics and impingement effects

Piesik, E. T.; Roberts, Dallas

doi:10.2514/3.29961

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A method to define low-altitude rocket exhaust characteristics and impingement effects

Cited by 6 publications

References 5 publications

Numerical simulation and field testing of flame-jet thermal spallation drilling—1. Model development

Numerical simulation and field testing of flame-jet thermal spallation drilling—1. Model development

Numerical simulation and field testing of flame-jet thermal spallation drilling—2. Experimental verification

Flowfield produced by rocket exhaust impingement of a multitube launcher

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