PRELIMINARY DESIGN ASPECTS OF MILITARY AIRCRAFT
Abstract
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; Designer's view of power plant problems; The design process; L' integration du propulseur et de la cellule sur un avion de combat supersonique; Designer's 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 designer's view of the systems integration problem; Development planning and operational capabilities.
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 01, 1970
- Accession Number
- AD0705370
Entities
Organizations
- AGARD