Modeling, Simulation and Hyprid Optimization Method as Design Tools for Range Extension Kit of a Subsonic Flying Body
Author:
Affiliation:
1. Military Technical College
2. Modern Sciences and Arts University
3. Cairo University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-0429
Reference13 articles.
1. Aerodynamic Design of an Extended Range Bomb
2. The Search for the Optimal Wing Configuration for Small Subsonic Air Vehicles
3. Parametric Study of Box-Wing Aerodynamics for Minimum Drag Under Stability and Maneuverability Constraints
4. Aero-structural approach coupled with direct operative cost optimization for new aircraft concept in preliminary design
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