Author: Massachusetts Institute of Technology. Department of Electrical Engineering. Center of AnalysisPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 154
Book Description
Tables of Supersonic Flow Around Cones of Large Yaw
Author: Massachusetts Institute of Technology. Department of Electrical Engineering. Center of AnalysisPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 154
Book Description
Tables of Supersonic Flow Around Yawing Cones
Author: Massachusetts Institute of Technology. Department of Electrical Engineering. Center of AnalysisPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 321
Book Description
Tables for Supersonic Flow Around Right Circular Cones at Small Angle of Attack
Author: Joseph L. SimsPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 440
Book Description
Tables of Supersonic Flow Around Yawing Cones
Author: MASSACHUSETTS INST OF TECH CAMBRIDGE CENTER OF ANALYSIS.Publisher:
ISBN:
Category :
Languages : en
Pages : 336
Book Description
Contents: Tables of supersonic flow of air around slightly yawing cones of the following semi-apex angles; Survey of the results; Table giving the shock-to-cone ratio in terms of the radial velocity-component along the solid surface and the semi-apex angle of the cone; Table giving the coefficient of normal drag in terms of the radial velocity-component along the solid surface and the semi-apex angle of the cone; Diagrams illustrating some physical properties of supersonic flow of air around slightly yawing cones.
Tables for Supersonic Flow Around Right Circular Cones at Zero Angle of Attack
Author: Joseph L. SimsPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 436
Book Description
Tables for Supersonic Flow Around Right Circular Cones at Zero Angle of Attack
Author: Joseph L. SimsPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 428
Book Description
Tables for Supersonic Flow Around Right Ciruclar Cones at Zero Angle of Attack
Author: Joseph L. SimsPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 444
Book Description
Tables of Supersonic Flow Around Cones of Large Yaw by the Staff of the Computing Section Center of Analysis Under the Direction of Zdeněk Kopal
Author: Tables for Supersonic Flow of Helium Around Right Circular Cones at Zero Angle of Attack
Author: Joseph L. SimsPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 36
Book Description
The results of the calculation of supersonic flow of helium about right circular cones at zero angle of attack are presented in tabular form. The calculations were performed using the Taylor-Maccoll theory. Numerical integrations were performed using a Runge-Kutta method for second-order differential equations. Results were obtained for cone angles from 2.5 to 30 degrees in regular increments of 2.5 degrees. In all calculations the desired free-stream Mach number was obtained to five or more significant figures.
Supersonic Flow Around Right Circular Cones, Tables for Zero Angle of Attack
Author: Joseph L. SimsPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 882
Book Description