Gulfstream II business jet is low wing aircraft of moderate sweep featuring T-tail arrangement and two aft-mounted turbofan engines; aerodynamic development of configuration and control system; significant design and aerodynamic characteristics with appropriate experimental data including force, pressure, and flow visualization results; wing optimization to meet requirements of high and low speed performance and pitch-down stall break at all flight conditions while providing adequate fuel volume; nacellepylon-wing relationship for optimum drag, engine characteristics, and airplane balance; empennage arrangement providing satisfactory stability and control of all conceivable flight conditions.
Gulfstream II aerodynamic design
SAE -- Paper
SAE Meeting ; 1967 ; United States , Wichita, KS Jet propelled
1967
10 pages
Aufsatz (Konferenz)
Englisch
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Gulfstream II Aerodynamic Design
SAE Technical Papers | 1967
|Online Contents | 2012
Online Contents | 2012