Author: Martin ZlotnickPublisher:
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 ZlotnickPublisher:
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
Author: Martin ZlotnickSubject Index to Unclassified ASTIA Documents
Author: Defense Documentation Center (U.S.)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 ZlotnickPublisher:
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. McVeighPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 236
Book Description
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 932
Book Description
NASA Contractor Report
Author: A Study of NACA and NASA Published Information of Pertinence in the Design of Light Aircraft
Author: James C. WilliamsPublisher:
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. CallaghanPublisher:
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. MendenhallPublisher:
ISBN:
Category : Interference (Aerodynamics)
Languages : en
Pages : 100
Book Description