Add to ORKGResults are presented for the moments and position of force centers of a series of cambered round bodies derived from a torpedo-like body of revolution. The effects of placing fins on the rear of the body of revolution are also included
The aerodnamic characteristics for several bodies of revolution have been determined from wind tunne...
The present series of studies is concerned with low-Reynolds-number flow in general; the main object...
Yawing-moment coefficients were obtained for several dorsal-fin and vertical-tail configurations in ...
Results are presented for the moments and position of force centers of a series of cambered round bo...
Effect of camber on aerodynamic characteristics of ogive-circular-cylindrical body at mach 2.0
To aid in assessing effects of cross-sectional shape on body aerodynamics, the forces and moments ha...
Static force and moment coefficients were measured in the High Speed Water Tunnel on nonpowered mode...
The forces and moments which act on a submerged body undergoing unsteady motion can be described in ...
Aerodynamic characteristics of bodies of revolution at Mach numbers from 1.50 to 2.86 and angles of ...
Results of tests to determine the aerodynamic forces and moments on bodies of revolution at angles o...
A SWATH configuration, consisting of twin submerged axially symmetric hulls and slender vertical str...
A series of tests were performed in the High Speed and Free Surface Water Tunnels to measure the for...
An experimental investigation was conducted to measure the static aerodynamic characteristics for tw...
For a body of revolution with afterbody side strakes, an experimental investigation was conducted in...
Massachusetts Institute of Technology. Dept. of Naval Architecture and Marine Engineering. Thesis. 1...
The aerodnamic characteristics for several bodies of revolution have been determined from wind tunne...
The present series of studies is concerned with low-Reynolds-number flow in general; the main object...
Yawing-moment coefficients were obtained for several dorsal-fin and vertical-tail configurations in ...
Results are presented for the moments and position of force centers of a series of cambered round bo...
Effect of camber on aerodynamic characteristics of ogive-circular-cylindrical body at mach 2.0
To aid in assessing effects of cross-sectional shape on body aerodynamics, the forces and moments ha...
Static force and moment coefficients were measured in the High Speed Water Tunnel on nonpowered mode...
The forces and moments which act on a submerged body undergoing unsteady motion can be described in ...
Aerodynamic characteristics of bodies of revolution at Mach numbers from 1.50 to 2.86 and angles of ...
Results of tests to determine the aerodynamic forces and moments on bodies of revolution at angles o...
A SWATH configuration, consisting of twin submerged axially symmetric hulls and slender vertical str...
A series of tests were performed in the High Speed and Free Surface Water Tunnels to measure the for...
An experimental investigation was conducted to measure the static aerodynamic characteristics for tw...
For a body of revolution with afterbody side strakes, an experimental investigation was conducted in...
Massachusetts Institute of Technology. Dept. of Naval Architecture and Marine Engineering. Thesis. 1...
The aerodnamic characteristics for several bodies of revolution have been determined from wind tunne...
The present series of studies is concerned with low-Reynolds-number flow in general; the main object...
Yawing-moment coefficients were obtained for several dorsal-fin and vertical-tail configurations in ...