Author: WIlliam R. Bates
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 538
Book Description
The aerodynamic characteristics of 19 isolated tail surfaces have been determined by wind-tunnel tests and tests have also been made of rectangular airfoils of various aspect ratios with and without double end plates of various shapes. Thes data from these tests have been collected and analyzed.
Collection and Analysis of Wind-tunnel Data on the Characteristics of Isolated Tail Surfaces with and Without End Plates
Author: WIlliam R. Bates
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 538
Book Description
The aerodynamic characteristics of 19 isolated tail surfaces have been determined by wind-tunnel tests and tests have also been made of rectangular airfoils of various aspect ratios with and without double end plates of various shapes. Thes data from these tests have been collected and analyzed.
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 538
Book Description
The aerodynamic characteristics of 19 isolated tail surfaces have been determined by wind-tunnel tests and tests have also been made of rectangular airfoils of various aspect ratios with and without double end plates of various shapes. Thes data from these tests have been collected and analyzed.
Applied Mechanics Reviews
A Selected Listing of NASA Scientific and Technical Reports for ...
Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1370
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1370
Book Description
Technical Note
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 876
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 876
Book Description
A Biharmonic Relaxation Method for Calculating Thermal Stress in Cooled Irregular Cylinders
Author: Arthur G. Holms
Publisher:
ISBN:
Category : Cylinders
Languages : en
Pages : 700
Book Description
A numerical method was developed for calculating thermal stresses in irregular cylinders cooled by one or more internal passages. The use of relaxation methods and elementary methods of finite differences was found to give approximations to the correct values when compared with previously known solutions for concentric circular cylinders possessing symmetrical and asymmetrical temperature distributions.
Publisher:
ISBN:
Category : Cylinders
Languages : en
Pages : 700
Book Description
A numerical method was developed for calculating thermal stresses in irregular cylinders cooled by one or more internal passages. The use of relaxation methods and elementary methods of finite differences was found to give approximations to the correct values when compared with previously known solutions for concentric circular cylinders possessing symmetrical and asymmetrical temperature distributions.
NASA Technical Note
Analytical Method of Determining Transmission of Particles and Radiation Through Great Thickness of Matter
Author: A. R. Bobrowsky
Publisher:
ISBN:
Category : Mathematical analysis
Languages : en
Pages : 668
Book Description
A matrixc method of determining transmission, scattering, and absorption of radition, such as gamma rays and neutrons, is presented in this report.
Publisher:
ISBN:
Category : Mathematical analysis
Languages : en
Pages : 668
Book Description
A matrixc method of determining transmission, scattering, and absorption of radition, such as gamma rays and neutrons, is presented in this report.
List of Technical Notes, 1947-1953
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 162
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 162
Book Description