Accession Number : AD0800541
Title : SUPERSONIC TRANSPORT PROGRAM PHASE II-C.
Descriptive Note : Monthly technical progress rept.
Corporate Author : BOEING CO RENTON WA
Report Date : NOV 1965
Pagination or Media Count : 160
Abstract : Significant progress accomplished on the SST program during October and November is summarized. Increases to the body depth are being studied as a means of increasing cargo and fuel volume. A comprehensive airport compatibility study is nearing completion. Good progress is being made in developing an understanding of the roll performance requirements of the SST. Four major Preliminary Design Reviews to evaluate design concepts were conducted. Repair of the full-scale test pivot bearing lug has been completed. Six wing specimens were flutter tested in the Boeing supersonic wind tunnel. A series of 1/10 scale inlet performance tests have been completed.
Descriptors : *SUPERSONIC AIRCRAFT), (*JET TRANSPORT PLANES, FLUTTER, WIND TUNNEL MODELS, LANDING GEAR, PERFORMANCE(ENGINEERING), ATTITUDE CONTROL SYSTEMS, ROLL, AIRPORTS, COMPATIBILITY, FLUID DYNAMICS, STRUCTURAL PROPERTIES, TURBOJET INLETS, FLIGHT CONTROL SYSTEMS, AERODYNAMIC LOADING, COST EFFECTIVENESS, TITANIUM COMPOUNDS, PAINTS, TURBOFAN ENGINES, AERODYNAMIC CHARACTERISTICS, TURBOJET ENGINES, VARIABLE SWEEP WINGS.
Subject Categories : Aerodynamics
Structural Engineering and Building Technology
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE