Box 18
Container
Contains 114 Results:
On the question of fanning oscillations during the flight of an uncontrolled R-body
File — Box: 18, Folder: (No Number)
Dates:
1920 - 1970
Flying body with guidance displacement for the purpose of pressure point relocation
File — Box: 18, Folder: (No Number)
Dates:
1920 - 1970
The Prandtl-Busemann approximation method for the drawing tracing of plane overflow flows, 1st theoretical part, 1940-08-21
File — Box: 18, Folder: (No Number)
Dates:
1940-08-21
The Prandtl-Busemann approximation method for the drawing tracking of plane overflow flows, 2. Practical application, 1940-08-21
File — Box: 18, Folder: (No Number)
Dates:
1940-08-21
Report on three-component measurements on the A4 model in the supersonic wind tunnel of the Peenemünde army test site, 1940-10-10
File — Box: 18, Folder: (No Number)
Dates:
1940-10-10
Report on three-component measurements with the A4 V12/a and A4 V12/c glider models, 1940-11-27
File — Box: 18, Folder: (No Number)
Dates:
1940-11-27
The Prandtl-Busemann approximation method for the graphical tracking of plane supersonic flows, 3rd basic features and implementation of the correction of wind tunnel nozzles., 1941-02-04
File — Box: 18, Folder: (No Number)
Dates:
1941-02-04
Comparative orbital calculations of the propellant mirror long bullet Lg 5/5 and the 28 cm grenade 35., 1941-03-17
File — Box: 18, Folder: (No Number)
Dates:
1941-03-17
Three-component measurements on a 5 cm high-explosive grenade L/4.5 and an explosive grenade for device 58 L/4.7 in the supersonic wind tunnel of the Peenemünde Army Test Site, 1941-03-15
File — Box: 18, Folder: (No Number)
Dates:
1941-03-15
Activity report of the Aerodynamic Main Department for the year 1940, 1941-01-10
File — Box: 18, Folder: (No Number)
Dates:
1941-01-10