Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 110
Book Description
Calculation of Turbulent Boundary Layers with Heat Transfer and Pressure Gradient Utilizing a Compressibility Transformation. Part 3: Computer Program Manual
Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 110
Book Description
Heat Transfer to Boundary Layers with Pressure Gradients
Author: Ralph Alois SebanPublisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 194
Book Description
Calculation of Turbulent Boundary Layers with Heat Transfer and Pressure Gradient Utilizing a Compressibility Transformation
Author: J. SchneiderPublisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 106
Book Description
A computer program is described capable of determining the properties of a compressible turbulent boundary layer with pressure gradient and heat transfer. The program treats the two-dimensional problem assuming perfect gas and Crocco integral energy solution. A compressibility transformation is applied to the equation for the conservation of mass and momentum, which relates this flow to a low speed constant property flow with simultaneous mass transfer and pressure gradient. The resulting system of describing equations consists of eight ordinary differential equations which are solved numerically. For Part 1, see N72-12226; for Part 2, see N72-15264.
Scientific and Technical Aerospace Reports
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1572
Book Description
Analytic Methods in Aircraft Aerodynamics
Author: Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 758
Book Description
Approximations for the Thermodynamic and Transport Properties of High-temperature Air
Author: C. Frederick HansenPublisher:
ISBN:
Category : Air
Languages : en
Pages : 724
Book Description
The thermodynamic and transport prorerties of high-temperature air are found in closed form starting from approximate partition functions for the major components in air and neglecting all minor components. The compressibility, energy, entropy, the specific heats, the speed of sound, the coefficients of viscosity and of thermal conductivity, and the Prandtl numbers for air are tabulated from 500 degrees to 15,000 degrees K over a range of pressure from 0.0001 to 100 atmospheres. The enthalpy of air and the mol fractions of the major components of air can easily be found from the tabulated values for compressibility and energy. It is predicted that the Prandtl number for fully ionized air will become small compared to unity, the order of 0.01, and this implies that boundary layers in such flow will be very transparent to heat flux.
Monthly Catalog of United States Government Publications, Cumulative Index
Author: United States. Superintendent of DocumentsPublisher:
ISBN:
Category : United States
Languages : en
Pages : 1408
Book Description
The Aerothermodynamics of Aircraft Gas Turbine Engines
Author: Gordon C. OatesPublisher:
ISBN:
Category : Aerothermodynamics
Languages : en
Pages : 830
Book Description
Applied Mechanics Reviews
Author: Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 628
Book Description
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1216
Book Description
