Defense Technical Information Center (DTIC) · 1961 · 34 citations · 3 references
AeroacousticsEngineeringLeadingedge BluntnessFluid MechanicsMechanical EngineeringSimplified Theoretical ApproachesComputational MechanicsBoundary LayerUnsteady FlowCompressible FlowPhysical AcousticNumerical SimulationSound PropagationHypersonic FlowBoundary Element MethodPhysicsIncompressible FlowFree Boundary ProblemMultiphase FlowBoundary-layer Self-induced PressuresSupersonic CombustionSimple SolutionsAerospace EngineeringCivil EngineeringStream Pressure GradientsAerodynamics
Simplified theoretical approaches are shown, based on hypersonic similarity boundary-layer theory, which allow reasonably accurate estimates to be made of the surface pressures on plates on which viscous effects are important. The consideration of viscous effects includes the cases where curved surfaces, stream pressure gradients, and leadingedge bluntness are important factors.
3
The Blunt Plate In Hypersonic Flow
Donald L. Baradell, M. H. Bertram · NASA Technical Reports Server (NASA) · 1960 · 15 citations · Full text