SUPERSONIC TRANSPORT DEVELOPMENT PROGRAM. PHASE III PROPOSAL. BOEING MODEL 2707. VOLUME II-7. AIRFRAME DESIGN REPORT. PART C. DESIGN CRITERIA LOADS. AERODYNAMIC HEATING FLUTTER
Abstract
This report presents the Boeing proposal for structural design loads and environment on the B-2707 commercial supersonic transport. Information on Phase III planning is included to define an efficient program necessary for first flight of the B-2707 prototype. Flight and ground loads criteria, flutter and vibration criteria, and structural design criteria are presented. The design loads and methods of analysis together with load validation data are presented in Sec. 3.0. The effects of these loads on ride comfort of the passengers and crew are also included. Structural temperature analyses that define the effects of aerodynamic and engine-induced heating on all major structure are presented in Sec. 4.0.
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 06, 1966
- Accession Number
- AD0804728
Entities
People
- D. R. Donaldson
Organizations
- Boeing