Vulnerability prediction method for use in aircraft conceptual design

Aeronautical Journal

Volumn 103, Issue 1024, 1999, Pages 309-315

  Al Ahmed, S ^a   Fielding, J P ^b  

^a King faisal Specialist   (Saudi Arabia)

^b NONE

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER AIDED DESIGN; COMPUTER SIMULATION;

AIRCRAFT CONCEPTUAL DESIGN;

AIRCRAFT;

EID: 0032687585     PISSN: 00019240     EISSN: None     Source Type: Trade Journal    
DOI: 10.1017/S0001924000064903     Document Type: Article

References (8)

1. RAYMER, D.P. Aircraft Design: A Conceptual Approach. AIAA Education Series. AIAA, Washington DC, 1989.
2. SIEGERS, F. Conceptual Design Synthesis and Optimisation for New Generations of Combat Aircraft. PhD. thesis, Cranfield University, 1996.
3. SCHRAGE, D.P. and MAVRIS, D.N. Integrated design and manufacturing for the high speed civil transport. AIAA-93/3994, AIAA, Washington, DC, 1993.
4. MIL-STD-2069, Requirements for Aircraft Non-nuclear Survivability Program. US Department of Defence, Washington.
5. BALL, R. Fundamentals of Aircraft Survivability, AIAA Educational Series, AIAA, Washington DC, 1988.
6. Parasolid Programming Reference Manual, Electronic Data Systems, Electronic Data Systems Corp. UK, Cambridge, UK, 1992.
7. GLASSNER, A.S. An Introduction to Ray Tracing, Academic Press, 1989.
8. AL-AHMED, S.M. Integraling Combat Effectiveness Disciplines into the Aircraft Conceptual/Preliminary Design, Phase. PhD Thesis. Cranfield University, 1996.