Object 68/1 - 68/40
Container
Contains 33 Results:
Report No. 1/40 TA/Proj. Estimation of the total polars for the 25 to glider (1st draft), 1940-02-23
File — Object: 68/1 - 68/40, Folder: Arch 68/1
Dates:
1940-02-23
Preliminary calculation of the supporting structure of the wing sockets of the 25 t glider, 1940-05-04
File — Object: 68/1 - 68/40, Folder: Arch 68/2
Dates:
1940-05-04
The report consists of 6 pages of text, 5 charts, 1940-04-27
File — Object: 68/1 - 68/40, Folder: Arch 68/3
Dates:
1940-04-27
Strength investigation of the 25 ton furnace in different versions, 1940-04-30
File — Object: 68/1 - 68/40, Folder: Arch 68/5 (Copy)
Dates:
1940-04-30
Trajectories of unit 4 for different deflections at burnout as a comparison to glider A4, 1940-05-23
File — Object: 68/1 - 68/40, Folder: Arhc 68/6
Dates:
1940-05-23
Trajectories of glider A4 at L = 0 degrees angle of attack after burn out, 1940-05-23
File — Object: 68/1 - 68/40, Folder: Arch 68/7
Dates:
1940-05-23
Report: 9/40: Trajectories of the glider A4 V12/u, 1940-09-26
File — Object: 68/1 - 68/40, Folder: Arch 66/8 (Copy)
Dates:
1940-09-26
Report: 9/40: Calculation of temperature for glider A4, 1940-11-09
File — Object: 68/1 - 68/40, Folder: Arch 68/9
Dates:
1940-11-09
Report 10/40: Aerodynamic underlays for gliders A4 V12/c, 1940-10-30
File — Object: 68/1 - 68/40, Folder: Arch 68/10
Dates:
1940-10-30
Report 10/41 TA/Proj.: Aerodynamic underlays for gliders A4 V12/c, 1941-03-15
File — Object: 68/1 - 68/40, Folder: Arch 68/11 (Copy)
Dates:
1941-03-15