Object 66/1 - 66/31
Container
Contains 30 Results:
2. Preliminary report on aerodynamic damping: Experimental determination of a dimensionless aerodynamic damping coefficient for a5 and A4 Clarification of the transfer laws from model tests to the original, 1939-10-18
File — Object: 66/1 - 66/31, Folder: Arch 66/16 (Copy)
Dates:
1939-10-18
Investigation of the effectiveness of the BE 11 airbrakes when unit 4 was in free flight., 1939-12-10
File — Object: 66/1 - 66/31, Folder: Arch 66/17
Dates:
1939-12-10
Report No. 18 on the applicability of an approximation formula derived in the 1st research report (Prof. Tollmien)., 1940-01-19
File — Object: 66/1 - 66/31, Folder: Arch 66/18 (Copy)
Dates:
1940-01-19
Report No. 19 resistance determination of the airbrakes Bk 1 - Bk 6 and Bk 11 (continuation of the report from 15.5.39), 1940-02-06
File — Object: 66/1 - 66/31, Folder: Arch 66/19 (Copy)
Dates:
1940-02-06
Report No. 20 Design of air rudders for spin stabilization of the A4, 1940-02-08
File — Object: 66/1 - 66/31, Folder: Arch 66/20
Dates:
1940-02-08
Report No. 21 on the mechanics of the vertical ascent of an R-body in a vacuum with views of the conditions in the air-filled space, 1940-03-02
File — Object: 66/1 - 66/31, Folder: Arch 66/21
Dates:
1940-03-02
Report No. 22 On the concept of entropy, 1940-02-27
File — Object: 66/1 - 66/31, Folder: Arch 66/22
Dates:
1940-02-27
Report No. 23, Influence of the jet on the aerodynamic properties of the A5 power unit, 1940-03-12
File — Object: 66/1 - 66/31, Folder: Arch 66/23
Dates:
1940-03-12
Report No. 24 The straight compression shock
File — Object: 66/1 - 66/31, Folder: Arch 66/24
Dates:
1920 - 1970
Report No. 25 Spin stabilization of the A4 using air rudders, taking into account an asymmetric tail unit, 1940-04-09
File — Object: 66/1 - 66/31, Folder: Arch 66/25 (Copy)
Dates:
1940-04-09