PRELIMINARY DESIGN ASPECTS OF MILITARY AIRCRAFT
ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (FRANCE)
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Contents Introductory paper Project design of combat aircraft Avions D arme - programmes et realisations The use of trade-off studies in preliminary design Aeroelastic constraints for large airplanes with a canard control Some fluid-dynamics considerations relating to the preliminary design of combat aircraft Future advances in the aerodynamics of military strike aircraft Designers view of power plant problems The design process L integration du propulseur et de la cellule sur un avion de combat supersonique Designers view of structural problems Load estimation and aeroelasticity in the initial stages of advanced combat aircraft design The influence of new materials on aircraft design Airframe systems design evaluation Etudes avancees dans le domaine de commandes de vol Advances in aircraft control systems with particular reference to combat aircraft The interface of maintainability, reliability, and associated disciplines in aircraft design Avionics designers view of the systems integration problem Development planning and operational capabilities.
- Attack and Fighter Aircraft