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Flugmechanik
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keywords:("Flugmechanik")
Pressure signature of an axisymmetric body at angle of attack.
Aerodynamic investigation of some high-drag entry shapes at Mach 15.4
Symmetrical, equilibrium flow past a blunt body at superorbital re-entry speeds.
Flow visualization of a secondary jet by means of lampblack injection techniques.
Effect of uncertainties in transport properties on prediction of stagnation-point heat transfer.
Three-dimensional flow calculation by the method of characteristics.
Wind-tunnel measurements of transition on the face of a blunt entry capsule at angle of attack.
Ablation patterns on cones having laminar and turbulent flows.
Boundary-layer transition on sharp cones at hypersonic Mach numbers.
Hypersonic transition studies on a slender cone at small angles of attack.
Prediction of lift and drag for slender sharp-edge delta wings in ground proximity