Author: John T. HowePublisher:
ISBN:
Category :
Languages : en
Pages : 80
Book Description
Solutions of the Laminar Compressible Boundary-layer Equations with Transpiration which are Applicable to the Stagnation Regions of Axisymmetric Blunt Bodies
Author: John T. HoweSolutions of the Laminar Compressible Boundary-layer Equations with Transpiration which are Applicable to the Stagnation Regions of Axisymmetric Blunt Bodies
Author: John T. HoweNASA Technical Note
Author: WADC Technical Report
Author: United States. Wright Air Development DivisionPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1356
Book Description
Radiation Shielding of the Stagnation Region by Transpiration of an Opaque Gas
Author: John T. HowePublisher:
ISBN:
Category : Gas dynamics
Languages : en
Pages : 28
Book Description
Applied Mechanics Reviews
Author: Monthly Catalog of United States Government Publications
Author: Preliminary Analysis of the Capabilities of a Composite Slab for an Advanced Heat-sink Design
Author: Paul A. LibbyPublisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 72
Book Description
Monthly Catalog of United States Government Publications, Cumulative Index
Author: United States. Superintendent of DocumentsPublisher:
ISBN:
Category : United States
Languages : en
Pages : 1300
Book Description
Stagnation-point Flow of a Variable-property Fluid at Low Reynolds Numbers
Author: Michael LenardPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 360
Book Description
Steady, viscous, two-dimensional and axially symmetric stagnation-point flows of a gas are considered for the case when the Reynolds number is too low for the applicability of the classical boundary-layer theory. It is assumed that the low-density gas is still a continuous fluid, permitting the use of the Navier-Stokes and as associated equations as the basis of the problem. The effects of low Reynolds number are determined by applying an expansion procedure to the fluid dynamical equations.