University of North Texas Digital Library (University of North Texas) · 1957 · 17 citations · 0 references
Open access
EngineeringAerospace EngineeringAerodynamicsComputational Fluid DynamicsComputational MechanicsHypersonic AerodynamicsShock WavesDetached Shock WavesMach NumberShock DynamicsShock Wave ModelingShock Wave PropagationShock Wave Structure
A reexamination has been made of the use of simple concepts for predicting the shape and location of detached shock waves. The results show that simple concepts and modifications of existing methods can yield good predictions for many nose shapes and for a wide range of Mach numbers.