Laminar Heat Transfer to a Swept Leading Edge in Hypersonic Flow
1967
228 pages
Report
Keine Angabe
Englisch
Fluid Mechanics , Structural Mechanics , Sweptback wings , Heat transfer , Aerodynamic heating , Leading edges , Hypersonic characteristics , Laminar flow , Blunt bodies , Turbulent boundary layer , Three dimensional flow , Compressible flow , Angle of attack , Perturbation theory , Flow fields , Equations of state , Differential equations , Cylindrical bodies , Yaw , Theory , Pressure , Numerical methods and procedures , Prandtl number , Computer programs , Crossflow , Fortran , Ibm 7094 computers , Ibm 7090 computers , Lift to drag ratio
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