1. The projectile as ·submitted is quite unstable due to the location of the center of gravity so far aft of the nose. This condition could be greatly improved by making the nose of metal instead of plastic. The tests illustrate how intimately the position of the G.G. is related to stability. Only one of the changes tested failed to increase the stability of the projectile. 2. Extending the tail aft by means of a 1-1/2" boom will add greatly to stability without increasing the drag materially. The effect of this on the interior ballistics of the mortar has not been investigated. 3. A 1-5/16" diameter disc at the rear of the fins would give greater stability than the 1-1/2" boom, but the drag would be increased 70%. This increased d...
This report covers Water Tunnel tests made on a 2-inch diameter model of the Mk 53 Aircraft Depth Bo...
Resistance tests were conducted in the High Speed Water Tunnel on 2-in. diameter models of the 5-in....
A 1/5-scale model of the Republic x-84 airplane (Army Project MX-578) was tested in the Langley 300 ...
1. The projectile as ·submitted is quite unstable due to the location of the center of gravity so f...
This report covers tests of a 2" diameter model of the 3.5" Rotating Rocket. Five different designs...
This report covers water tunnel tests of a 2" diameter model of a 4.5" rocket projectile (designated...
This memorandum covers water Tunnel Tests of the 15 cm. German Spinner Rocket. The tests were made ...
This report covers tests of a 2" diameter model of the 7.2" Chemical Rocket to determine its perform...
This report is a supplement to Report Section No. 6.1-sr207-1270, dated April 21, 1944, and coves te...
The High Speed Water Tunnel is operated by the California Institute of Technology under Contract OEM...
The High Speed Water Tunnel is operated by the California Institute of Technology under Contract OEM...
This report covers water tunnel tests of a full scale 21 3/8" long rocket projectile (designed in th...
The high speed water tunnel was established at the California Institute of Technology to study the f...
This report covers the tests of a 2" diameter model of the 4. 5" H. E. Rocket, T38E3, to determine ...
This report covers tests on the M-6, 2.36" rocket with the conical pointed nose in combination with ...
This report covers Water Tunnel tests made on a 2-inch diameter model of the Mk 53 Aircraft Depth Bo...
Resistance tests were conducted in the High Speed Water Tunnel on 2-in. diameter models of the 5-in....
A 1/5-scale model of the Republic x-84 airplane (Army Project MX-578) was tested in the Langley 300 ...
1. The projectile as ·submitted is quite unstable due to the location of the center of gravity so f...
This report covers tests of a 2" diameter model of the 3.5" Rotating Rocket. Five different designs...
This report covers water tunnel tests of a 2" diameter model of a 4.5" rocket projectile (designated...
This memorandum covers water Tunnel Tests of the 15 cm. German Spinner Rocket. The tests were made ...
This report covers tests of a 2" diameter model of the 7.2" Chemical Rocket to determine its perform...
This report is a supplement to Report Section No. 6.1-sr207-1270, dated April 21, 1944, and coves te...
The High Speed Water Tunnel is operated by the California Institute of Technology under Contract OEM...
The High Speed Water Tunnel is operated by the California Institute of Technology under Contract OEM...
This report covers water tunnel tests of a full scale 21 3/8" long rocket projectile (designed in th...
The high speed water tunnel was established at the California Institute of Technology to study the f...
This report covers the tests of a 2" diameter model of the 4. 5" H. E. Rocket, T38E3, to determine ...
This report covers tests on the M-6, 2.36" rocket with the conical pointed nose in combination with ...
This report covers Water Tunnel tests made on a 2-inch diameter model of the Mk 53 Aircraft Depth Bo...
Resistance tests were conducted in the High Speed Water Tunnel on 2-in. diameter models of the 5-in....
A 1/5-scale model of the Republic x-84 airplane (Army Project MX-578) was tested in the Langley 300 ...