The objective of this study is to identify a reference configuration concept for 2 supersonic transports and the associated characteristics obtainable through the application of the results of recent research. This concept is a 292 passenger M 2.7 design with a subsonic leading edge wing and utilizes four dry turbojet engines for propulsion. The engines use the variable geometry turbine feature to reduce the engine-size required to meet the FAR 36 noise requirements. The wing geometry has been refined to provide improvements in stability and control, and performance indicated by extensive wind tunnel tests. The Boeing 1968 study concept is used as a base from which the current study concept and characteristics are developed. It is anticipated that the present reference study configuration will provide a reasonable baseline for future trade studies and for application of further technology improvements.
Advanced Supersonic Technology Concept Study Reference Characteristics
1973
307 pages
Report
No indication
English