Aerodynamic Engine/Airframe Integration for High Performance Aircraft and Missiles (L'Integration Aerodynamique des Moteurs et des Cellules dans les Avions et les Missiles a Hautes Performances)
Abstract
The 32 papers presented at the AGARD Fluid Dynamics Panel (FDP) symposium on 'Aerodynamic Engine/Airframe Integration for High Performance Aircraft and Missiles' that was held 7th-11th October 1991 in Fort Worth, Texas, United States are contained in this report. In addition to these papers, the Technical Evaluation Report aimed at assessing the relevance and success of the symposium in meeting the technical needs of the aerospace community and the transcript of the Round Table Discussion held at the end of the meeting are included in this document. The objective of the symposium was to review the state-of-art in aerodynamic engine/airframe integration techniques and to report on the progress which has been achieved during engineering project work in recent years. Because the treatment of this subject requires an interdisciplinary approach, both experimentalists and theoreticians were invited to contribute to the meeting. Six sessions were organized to cover the essential sub-disciplines requiring aerodynamic engine/airframe integration during the concept-assessment and design phases for new aerospace vehicles.
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1992
- Accession Number
- ADA257974
Entities
Organizations
- AGARD