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Tables of Supersonic Flow Around Cones of Large Yaw

Author: Massachusetts Institute of Technology. Department of Electrical Engineering. Center of Analysis
Publisher:
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 Analysis
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 154

Book Description

Supersonic Flow Around Cones at Large Yaw

Author: G. B. W. YOUNG
Publisher:
ISBN:
Category :
Languages : en
Pages : 43

Book Description
Equations were developed for the flow properties in the region bounded by a supersonic cone body at large angle of attack and its attached shock wave, for use with the tabulations of Kopal. A comparison of the theoretical results is made with the experimental data of Cronvich. A slight discrepancy which increases with increasing Mach number was found in the value of K sub DYH, the yawing head drag as tabulated by Kopal. (Author).

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:
Publisher:
ISBN:
Category :
Languages : en
Pages : 125

Book Description

Tables for Supersonic Flow Around Right Circular Cones at Zero Angle of Attack

Author: Joseph L. Sims
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 428

Book Description

Tables for Supersonic Flow Around Right Circular Cones at Small Angle of Attack

Author: Joseph L. Sims
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 440

Book Description

Tables of Supersonic Flow Around Yawing Cones

Author: Massachusetts Institute of Technology. Department of Electrical Engineering. Center of Analysis
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 376

Book Description

Correlation Graphs for Supersonic Flow Around Right Circular Cones at Zero Yaw in Air as a Perfect Gas

Author: Mitchel H. Bertram
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 32

Book Description
Concise accurate graphs of cone flow properties at zero yaw in air as a perfect gas are presented in correlation form. From these graphs the pressure, density, temperature, shock angle, and Mach number may be obtained both at the cone surface and immediately behind the shock, for free-stream Mach numbers from that for shock detachment to that approaching infinity and for cone semi -apex angles up to 50°. In addition, the initial slope of the normal-force curve is given for the same range of conditions.