Flexible multi-body design of a morphing UCAV

Collection of Technical Papers - AIAA 3rd "Unmanned-Unlimited" Technical Conference, Workshop, and Exhibit

Volumn 2, Issue , 2004, Pages 1053-1063

  Hong, Chul Hwa ^a,b   Cheplak, Matthew ^a,b   Choi, Jou Young ^a,b   Mavris, Dimitri N ^a  

^a GEORGIA INSTITUTE OF TECHNOLOGY   (United States)

^b Georgia Institute of Technology   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

MORPHING; MULTI-BODY DESIGN; UNMANNED AERIAL VEHICLES (UAV); UNMANNED COMBAT AERIAL VEHICLES (UCAV);

AIRCRAFT; ASPECT RATIO; FINITE ELEMENT METHOD; FLIGHT DYNAMICS; MISSILES; NATURAL FREQUENCIES; SENSORS;

UNMANNED VEHICLES;

EID: 19644394107     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (7)

1. DYMORE, Multi-body Structural Analysis Software, GaTech, Atlanta, GA, 2004 http://www.ae.gatech.edu/~obauchau/ [cited 4 April 2004].
2. Yurkovich, Rudolph N., "RFP for Morphing Aircraft and Morphing Aircraft Mission Analysis".
3. Niu, Michael C., Airframe Structural Design, Hong Kong Conmilit Press LTD.
4. Irian Ordaz, Lee, Kyong Hun, and Don M. Clark, "Aerodynamic Optimization Using Physics-Based Response Surface Methodology for a Multi-Mission Morphing Unmanned Combat Air Vehicle", Proceedings of AIAA 3rd "Unmanned Unlimited" Technical Conference, Workshop and Exhibit, Hilton Chicago, Chicago, Illinois, 2004, will publish
5. Tests, Impact, Shock absorber landing gear, Aircraft, MIL-T-6053C(USAF) 20 July 1977
6. th ed., Upper Saddle River, New Jersey
7. rd ed., AIAA Inc., Reston, Virginia, 1999