Design of a Rocket-Powered Descent Jetpack Equipped with Parachute
Author:
Affiliation:
1. Abu Dhabi University,Department of Mechanical Engineering,Abu Dhabi,UAE
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/9764877/9764959/09765066.pdf?arnumber=9765066
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1. ANSYS Fluent Theory Guide 18.0;fluent,2017
2. CFD Analysis of a Rocket Nozzle with FourInlets at Mach 2.1
3. CFD Analysis on a Different Advaned Rocket Nozzle;parthibha;International Journal of Enigneering and Advaned Technology (IJEAT),2015
4. A Mass Model for Liquid Propellant Rocket Engines
5. Aerodynamics Analysis of Grid Fins Inner Lattice Structure in Cruise Missile
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