A Study of the Blunt Slab Delta Wing at Hypersonic Speeds and Angles of Attack
1972
74 pages
Report
No indication
English
Fluid Mechanics , Aircraft , Delta wings , Flow fields , Hypersonic flow , Heat transfer , Three dimensional flow , Stagnation point , Entropy , Aerodynamic heating , Boundary layer , Airplane models , Sweptback wings , Blunt bodies , Wind tunnel models , Model tests , Lifting reentry vehicles , Pressure , Instrumentation , Pitot tubes , Oils , Flow visualization , Schlieren photography , Angle of attack , Vapors , Shock waves , Leading edges , Spark shadowgraph photography , Blunt slab delta wings , Cross flow theory , Slip lines(Aerodynamics) , Streamline divergence theory , Strip theory , Vapor screen flow visualization
Flow over a Delta Wing and Blunt Body Combination at Hypersonic Speeds
British Library Online Contents | 1994
|Flow over a Delta Wing and Blunt Body Combination at Hypersonic Speeds
British Library Conference Proceedings | 1994
|Surface pressure distribution at hypersonic speeds for blunt Delta wings at angle of attack
Engineering Index Backfile | 1959
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