Author: Joseph W. ClearyPublisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 82
Book Description
An Experimental and Theoretical Investigation of the Pressure Distribution and Flow Fields of Blunted Cones at Hypersonic Mach Number
Author: Joseph W. ClearyPublisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 82
Book Description
An Experimental and Theoretical Investigation of the Pressure Distribution and Flow Fields of Blunted Cones at Hypersonic Mach Numbers
Author: Joseph W. ClearyGovernment-wide Index to Federal Research & Development Reports
Author: Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1050
Book Description
Critical Evaluation of Transition from Laminar to Turbulent Shear Layers with Emphasis on Hypersonically Traveling Bodies
Author: Mark Vladimir Morkovin (|d)Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 152
Book Description
NASA Technical Note
Author: Proceedings of the Eighth Annual Thermal and Fluids Analysis Workshop: Spacecraft Analysis and Design
Author: A Method of Characteristics for Steady Three-dimensional Supersonic Flow with Application to Inclined Bodies of Revolution
Author: John V. RakichPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 68
Book Description
Characteristics method for determining three dimensional supersonic flow around inclined body of revolution.
Three-dimensional Laminar Boundary-layer Analysis of Upwash Patterns and Entrained Vortex Formation on Sharp Cones at Angle of Attack
Author: John C. Adams (Jr.)Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 124
Book Description
Application of three-dimensional inviscid and viscous (laminar boundary layer) analyses for cold wall hypersonic flows over sharp cones at incidence is presented relative to experimental data, showing surface upwash angles and entrained vortex formation leading to crossflow-induced boundary-layer transition. Three-dimensional neutral inviscid stability theory for stationary disturbances is used to calculate the angular orientation of the entrained vortices in the boundary layer while a maximum crossflow Reynolds number concept is applied for correlation of the onset to vortex formation due to crossflow instability.
Author: 
Author: