Object 66/32 - 66/54
Container
Contains 19 Results:
The Prandtl-Busemann approximation method for following plane supersonic flows in drawings II. Practical application, 1940-08-21
File — Object: 66/32 - 66/54, Folder: Arch 66/32
Dates:
1940-08-21
Report on three-component measurements on the A4 unit - model in the supersonic wind tunnel of the Peenemunde army test site, 1940-10-10
File — Object: 66/32 - 66/54, Folder: Arch 66/33 (Copy)
Dates:
1940-10-10
Report on three-component measurements with the models of gliders with A4 V12/a and A4 V12/c, 1940-11-27
File — Object: 66/32 - 66/54, Folder: Arch 66/34 (Copy)
Dates:
1940-11-27
The Prandtl-Busemannsche approximation procedure for the graphic following of planar supersonic flows III. Principles and implementation of the correction of wind tunnel nozzles, 1941-02-04
File — Object: 66/32 - 66/54, Folder: Arch 66/36
Dates:
1941-02-04
Comparative trajectory calculations of Lg 5/5 sabot long projectile and the 28 cm grenade 35, 1941-03-17
File — Object: 66/32 - 66/54, Folder: Arch 66/37 (Copy)
Dates:
1941-03-17
Three-component measurements on a 5 cm high-explosive grenade L/4.5 and a high-explosive grenade for the Device 58 L/4.7 in the supersonic wind tunnel of the Peenemunde army test site, 1941-03-15
File — Object: 66/32 - 66/54, Folder: Arch 66/38 (Copy)
Dates:
1941-03-15
Activity report of the main aerodynamic department for the year 1940, 1941-01-10
File — Object: 66/32 - 66/54, Folder: Arch 66/39
Dates:
1941-01-10
Flight path calculation of the A5 with air rudder control, 1941-05-08
File — Object: 66/32 - 66/54, Folder: Arch 66/40
Dates:
1941-05-08
Investigation of the design of a wind tunnel with continuous operation for sub- and supersonic speeds with the possible efficiency, 1941-05-06
File — Object: 66/32 - 66/54, Folder: Arch 66/41 (Copy)
Dates:
1941-05-06
Calculations for the planned dropping tests of the unit body A5 with brake flaps BK 11, 1941-07-21
File — Object: 66/32 - 66/54, Folder: Arch 66/45 (Copy)
Dates:
1941-07-21