A Simplified Mathematical Model For Calculating Aerodynamic Loading And Downwash For Midwing Wing Fuselage Combinations With Wings Of Arbitrary Plan Form PDF Download

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A Simplified Mathematical Model for Calculating Aerodynamic Loading and Downwash for Wing-fuselage Combinations with Wings

A Simplified Mathematical Model for Calculating Aerodynamic Loading and Downwash for Wing-fuselage Combinations with Wings
Author: Martin Zlotnick
Publisher:
Total Pages: 38
Release: 1954
Genre: Aerodynamic load
ISBN:

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In addition the report shows how the simplified mathematical model can be used for calculating the downwash behind the wing and for calculating the spanwise lift distribution on the wing for midwing configurations with axisymmetric fuselages.


NASA Contractor Report

NASA Contractor Report
Author:
Publisher:
Total Pages: 1012
Release: 1971
Genre: Aeronautics
ISBN:

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Analogy Between Mass and Heat Transfer with Turbulent Flow

Analogy Between Mass and Heat Transfer with Turbulent Flow
Author: Edmund E. Callaghan
Publisher:
Total Pages: 724
Release: 1953
Genre: Heat
ISBN:

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An analysis of combined heat and mass transfer from a flat plate has been made in terms of Prandtl's simpified physical concept of the turbulent boundary layer. The results of the analysis show that tor conditioins of reasonably small heat and mass transfer, the ratio of the mass- and heat-transfer coefficients is dependent on the Reynolds number of the boundary layer, the Prandtl number of the medium of diffusion, and the Schmidt number of the diffusing fluid in the medium of diffusion. For the particular case of water evaporating into air, the ratio of mass-transfer coefficient to heat-transfer coefficient is found to be slightly greater than unity.