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:
Published: 1953
Total Pages: 40
ISBN-13:
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Author: Martin Zlotnick
Publisher:
Published: 1953
Total Pages: 40
ISBN-13:
DOWNLOAD EBOOKAuthor: Defense Documentation Center (U.S.)
Publisher:
Published: 1960
Total Pages: 296
ISBN-13:
DOWNLOAD EBOOKAuthor: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1953
Total Pages: 932
ISBN-13:
DOWNLOAD EBOOKAuthor: M. A. McVeigh
Publisher:
Published: 1971
Total Pages: 236
ISBN-13:
DOWNLOAD EBOOKAuthor: James C. Williams
Publisher:
Published: 1970
Total Pages: 716
ISBN-13:
DOWNLOAD EBOOKThis report investigates critical reviews of NACA and NASA report literature on aerodynamics and aerodynamic load calculations for light aircraft design.
Author: M. R. Mendenhall
Publisher:
Published: 1971
Total Pages: 100
ISBN-13:
DOWNLOAD EBOOKAuthor: Edmund E. Callaghan
Publisher:
Published: 1953
Total Pages: 724
ISBN-13:
DOWNLOAD EBOOKAn 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.
Author:
Publisher:
Published: 1954
Total Pages: 910
ISBN-13:
DOWNLOAD EBOOKAuthor: Royal Aeronautical Society
Publisher:
Published: 1954
Total Pages: 938
ISBN-13:
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