The results of static force tests on a 2-in. diameter model of Weapon "A" in the High Speed Water Tunnel are presented. Drag coefficient was measured for Reynolds numbers from l.3 to 8.0 x 10^6 at zero degrees attack angle. Lift, drag, and pitching moment were measured as a function of attack angle for Reynolds numbers of 3.8 and 5.1 x 10^6
Wind-tunnel tests have been conducted to determine the errors of 3 seven static-pressure probes moun...
The test section of the High-Speed Water Tunnel (1) was modified in preparation for experiments on t...
Resistance tests were conducted in the High Speed Water Tunnel on 2-in. diameter models of the 5-in....
The results of static force tests on a 2-in. diameter model of Weapon "A" in the High Speed Water Tu...
The results of force tests of models of the Basic Finner missile configuration in fully wetted flow ...
Static force and moment coefficients were measured in the High Speed Water Tunnel on nonpowered mode...
Water tunnels have been utilized in one form or another to explore fluid mechanics and aerodynamics ...
The High Speed Water Tunnel is operated by the California Institute of Technology under Contract OEM...
The measurement of dynamic coefficients in a water tunnel is considered generally, and it is shown ...
Two-dimensional tests were conducted on a NACA 66(MOD) hydrofoil in the the GALCIT Hydrolab High Spe...
Force measurement runs were made on a model MK 13-2 Torpedo to correct previously reported results ...
The results of force tests on the NACA 66_(1-012) hydrofoil in noncavitating and cavitating two-dime...
An experimental program was initiated in the High Speed Water Tunnel to measure force coefficients f...
The measurement of model drag in the High Speed Water Tunnel has been difficult because of the inte...
Wind-tunnel tests have been conducted to determine the errors of 3 seven static-pressure probes moun...
Wind-tunnel tests have been conducted to determine the errors of 3 seven static-pressure probes moun...
The test section of the High-Speed Water Tunnel (1) was modified in preparation for experiments on t...
Resistance tests were conducted in the High Speed Water Tunnel on 2-in. diameter models of the 5-in....
The results of static force tests on a 2-in. diameter model of Weapon "A" in the High Speed Water Tu...
The results of force tests of models of the Basic Finner missile configuration in fully wetted flow ...
Static force and moment coefficients were measured in the High Speed Water Tunnel on nonpowered mode...
Water tunnels have been utilized in one form or another to explore fluid mechanics and aerodynamics ...
The High Speed Water Tunnel is operated by the California Institute of Technology under Contract OEM...
The measurement of dynamic coefficients in a water tunnel is considered generally, and it is shown ...
Two-dimensional tests were conducted on a NACA 66(MOD) hydrofoil in the the GALCIT Hydrolab High Spe...
Force measurement runs were made on a model MK 13-2 Torpedo to correct previously reported results ...
The results of force tests on the NACA 66_(1-012) hydrofoil in noncavitating and cavitating two-dime...
An experimental program was initiated in the High Speed Water Tunnel to measure force coefficients f...
The measurement of model drag in the High Speed Water Tunnel has been difficult because of the inte...
Wind-tunnel tests have been conducted to determine the errors of 3 seven static-pressure probes moun...
Wind-tunnel tests have been conducted to determine the errors of 3 seven static-pressure probes moun...
The test section of the High-Speed Water Tunnel (1) was modified in preparation for experiments on t...
Resistance tests were conducted in the High Speed Water Tunnel on 2-in. diameter models of the 5-in....