Ramjet powered missile design using a genetic algorithm

AIAA Paper

Volumn , Issue , 2004, Pages 814-824

  Hartfield, Roy J ^a,b   Jenkins, Rhonald M ^a,b   Burkhalter, John E ^a,b  

^a AUBURN UNIVERSITY   (United States)

^b Department of Aerospace Engineering ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTOR MODELING; CONE SHOCK SOLUTION; MACCOLL EQUATION; MISSILE DESIGN;

AEROSPACE ENGINEERING; COMBUSTORS; DEGREES OF FREEDOM (MECHANICS); ELECTRONIC EQUIPMENT; ENCODING (SYMBOLS); FLIGHT SIMULATORS; GENETIC ALGORITHMS; MACHINE DESIGN; NOZZLES; OPTIMIZATION;

MISSILES;

EID: 2942748362     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)

1. Anderson, M. B., Burkhalter, J. E. and Jenkins, R. M., "Design of a Guided Missile Interceptor Using Genetic Algorithms", Journal of Spacecraft and Rockets, Vol 38, No. 1, Jan. 2001
2. th AIAA Aerospace Science Meeting, Reno, NV, Jan. 2001.
3. th AIAA Aerospace Sciences Conference, Reno NV, Jan 1999.
4. nd Edition, McGraw-Hill, New York, NY, 1990, pp 294-306
5. NACA Report 1135, "Equations, Tables and Charts for Compressible Flow," Ames Research Staff, Ames Aeronautical Laboratory, Moffett Field, CA, 1953
6. Mattingly, Jack D., Elements of Gas Turbine Propulsion. McGraw Hill, 1996, pp.820- 822.