Numerical study of hot launch of missile inside a tube
Author:
Affiliation:
1. Directorate of Computational Dynamics, Defence Research and Development Laboratory, Hyderabad, India
Publisher
SAGE Publications
Subject
Mechanical Engineering,Aerospace Engineering
Link
http://journals.sagepub.com/doi/pdf/10.1177/0954410014522609
Reference15 articles.
1. Secondary Flows in a Rocket Launcher Tube
2. Experimental investigation of two-dimensional, supersonic flow impingement on a normal surface.
3. The Occurrence of Stagnation Bubbles in Supersonic Jet Impingement Flows
4. The impingement of underexpanded axisymmetric jets on wedges
5. Experimental Study of Underexpanded Supersonic Jet Impingement on an Inclined Flat Plate
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