Author: Martin Zlotnick
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 40
Book Description
A Simplified Mathematical Model for Calculating Aerodynamic Loading and Downwash for Midwing Wing-fuselage Combinations with Wings of Arbitrary Plan Form
Author: Martin Zlotnick
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 40
Book Description
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 40
Book Description
A Simplified Mathematical Model for Calculating Aerodynamic Loading and Downwash for Wing-fuselage Combinations with Wings of Arbitrary Plan Form
Subject Index to Unclassified ASTIA Documents
Author: Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 296
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 296
Book Description
A Simplified Mathematical Model for Calculating Aerodynamic Loading and Downwash for Wing-fuselage Combinations with Wings
Author: Martin Zlotnick
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 38
Book Description
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.
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 38
Book Description
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.
A Design Summary of Stall Characteristics of Straight Wing Aircraft
Author: M. A. McVeigh
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 236
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 236
Book Description
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 932
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 932
Book Description
NASA Contractor Report
A Study of NACA and NASA Published Information of Pertinence in the Design of Light Aircraft
Author: James C. Williams
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 716
Book Description
This report investigates critical reviews of NACA and NASA report literature on aerodynamics and aerodynamic load calculations for light aircraft design.
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 716
Book Description
This report investigates critical reviews of NACA and NASA report literature on aerodynamics and aerodynamic load calculations for light aircraft design.
Analogy Between Mass and Heat Transfer with Turbulent Flow
Author: Edmund E. Callaghan
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 724
Book Description
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.
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 724
Book Description
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.
Theoretical Investigation of the Aerodynamic Interference Induced by Cruise and Lift Fans on Transport-type Aircraft
Author: M. R. Mendenhall
Publisher:
ISBN:
Category : Interference (Aerodynamics)
Languages : en
Pages : 100
Book Description
Publisher:
ISBN:
Category : Interference (Aerodynamics)
Languages : en
Pages : 100
Book Description