Box 18
Container
Contains 114 Results:
Report No. 18: On the applicability of an approximation derived in the 1st research report (Prof. Tollmien), 1940-01-19
File — Box: 18, Folder: (No Number)
Dates:
1940-01-19
Report No. 19: Determination of the resistance of the butterfly valves Bk 1 - Bk 6 and Bk 11 (continuation of the report of 15.5.39), 1940-02-06
File — Box: 18, Folder: 66/19 (UAH)
Dates:
1940-02-06
Report No. 20: Design of air rudders for the spin stabilization of the A4.
File — Box: 18, Folder: (No Number)
Dates:
1920 - 1970
Report No. 22: On the concept of entropy. Contents report, 1940-02-27
File — Box: 18, Folder: (No Number)
Dates:
1940-02-27
Report No. 23: Influence of the engine on the aerodynamic properties of the A5 unit., 1940-03-12
File — Box: 18, Folder: (No Number)
Dates:
1940-03-12
Report 24: The Straight Compression Kick Table of Contents, 1940-05-08
File — Box: 18, Folder: (No Number)
Dates:
1940-05-08
Report 25: The spin stabilization of the A4 by air rudder taking into account a tail unit asymmetry, 1940-04-09
File — Box: 18, Folder: (No Number)
Dates:
1940-04-09
2. Continuation of the weighting on bromine flaps from 15.5.35 - AA/FL No. 8, ejection tests
File — Box: 18, Folder: 66/26 (UAH)
Dates:
1920 - 1970
Three-component wind tunnel measurements on 15 cm DOV projectiles (according to drawing R I C 559 Wa Test 11/I), 1940-07-17
File — Box: 18, Folder: (No Number)
Dates:
1940-07-17
Preliminary report on measurements with the A4 V12/a glider, 1940-07-26
File — Box: 18, Folder: (No Number)
Dates:
1940-07-26