Box 25
Container
Contains 91 Results:
Reel-C 1840 A.T.I. 1819 Applicability of an Approximation Expression derived by Prof. Tollmien, 1819
File — Box: 25, Folder: Arch 66/18
Dates:
1819
Reel-C 944 A.T.I. 1820 RESTRICTED Report No. 19 Resistance determination of airbrakes Bk 1 - Bk 6 and Bk 11, 1940-02-06
File — Box: 25, Folder: Arch 66/19
Dates:
1940-02-06
A.T.I. 1826 UNCLASSIFIED Spin Stabilization of the A4 with Air Rudder taking into consideration tail assembly asymmetry, 1948-10-07
File — Box: 25, Folder: Arch 66/25
Dates:
1948-10-07
A.T.I. 1827 UNCLASSIFIED Second Continuation of Report No.8, on Braking Flaps of May 15, 1939 AA/F, 1939-06
File — Box: 25, Folder: Arch 66/26
Dates:
1939-06
About the occurrence of oscillations during the flight of an uncontrolled missile, 1940-08-03
File — Box: 25, Folder: Arch 66/29
Dates:
1940-08-03
Flying body with shiftable fins in order to move the cneter of pressure (records for an application for a patent), 1940-08-19
File — Box: 25, Folder: Arch 66/30
Dates:
1940-08-19
Study of three-component-measurements obtained from an a4 type model in the supersonic wind tunnel
File — Box: 25, Folder: arch 66/33
Dates:
1920 - 1970
Report on three-component tests on the glider models A4 V12/a & a4 V12/o, 1940-11-27
File — Box: 25, Folder: Arch 66/34 (Translation)
Dates:
1940-11-27
A.T.I. 1837 UNCLASSIFIED 1837 Comparative path calculations of the disk-driven long missile lg 5/5 and the 28 cm. grenade 35, 1941-03
File — Box: 25, Folder: Arch 66/37
Dates:
1941-03
A.T.I. 1838 UNCLASSIFIED Three component tests on 5 cm high explosive shells, 1941-03
File — Box: 25, Folder: Arch 66/38
Dates:
1941-03