Author: H. Reese Ivey
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 28
Book Description
A method is developed for calculating the pressures on aerodynamic shapes at very high supersonic speeds in dense air with the ratio of specific heats equal to 1. The method is applicable to any body of revolution at zero angle of attack and to any two-dimensional profile. The results of the present paper are compared with previous work of Von Karman and Epstein on this problem and the difference explained.
A Method for Determining the Aerodynamic Characteristics of Two- and Three-dimensional Shapes at Hypersonic Speeds
Author: H. Reese Ivey
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 28
Book Description
A method is developed for calculating the pressures on aerodynamic shapes at very high supersonic speeds in dense air with the ratio of specific heats equal to 1. The method is applicable to any body of revolution at zero angle of attack and to any two-dimensional profile. The results of the present paper are compared with previous work of Von Karman and Epstein on this problem and the difference explained.
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 28
Book Description
A method is developed for calculating the pressures on aerodynamic shapes at very high supersonic speeds in dense air with the ratio of specific heats equal to 1. The method is applicable to any body of revolution at zero angle of attack and to any two-dimensional profile. The results of the present paper are compared with previous work of Von Karman and Epstein on this problem and the difference explained.
A Method for Determining the Aerodynamic Characteristics of Two- and Three-dimensional Shapes at Hypersonic Speeds
Author: F. Reese Ivey
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 21
Book Description
Some aerodynamic characteristics of several shapes are calculated, and it is shown that the lift and drag coefficients are dependent upon the thickness ratio, thickness distribution, and angle of attack.
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 21
Book Description
Some aerodynamic characteristics of several shapes are calculated, and it is shown that the lift and drag coefficients are dependent upon the thickness ratio, thickness distribution, and angle of attack.
Technical Note
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
Book Description
NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 2300
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 2300
Book Description
Report
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 40
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 40
Book Description
Experimental Pressure Distributions Over Blunt Two- and Three-dimensional Bodies Having Similar Cross Sections at a Mach Number of 4.95
Author: Jerome D. Julius
Publisher:
ISBN:
Category :
Languages : en
Pages : 22
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 22
Book Description
Theoretical and Analog Studies of the Effects of Nonlinear Stability Derivatives on the Longitudinal Motions of an Aircraft in Response to Step Control Deflections and to the Influence of Proportional Automatic Control
Author: Benjamin Milwitzky
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 348
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 348
Book Description
The Effect of Blade-section Thickness Ratios on the Aerodynamic Characteristics of Related Full-scale Propellers at Mach Numbers Up to 0.65
Author: A. J. Eggers
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 286
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 286
Book Description
Report
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 962
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 962
Book Description
A Selected Listing of NASA Scientific and Technical Reports for ...
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 664
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 664
Book Description