Aerodynamic Shape Optimization of Payload Fairing Boat Tail for Various Diameter Ratios
Author:
Affiliation:
1. Indian Institute of Space Science and Technology, Thiruvananthapuram 695 547, Kerala, India
2. Indian Space Research Organization, Thiruvananthapuram 695 022, Kerala, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A35215
Reference12 articles.
1. Computational-Fluid-Dynamics-Based Design Optimization of a Large Asymmetric Payload Fairing
2. Multi-Objective Multidisciplinary Design Optimization Approach for Partially Reusable Launch Vehicle Design
3. Missile Aerodynamic Shape Optimization Using Genetic Algorithms
4. Multiobjective Optimization of Earth-Entry Vehicle Heat Shields
5. Flowfield study over a bulbous payload shroud in transonic and low supersonic Mach number
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