Object 66/84 - 66/115
Container
Contains 22 Results:
Three-component measurements on glider A4 V12/f, 1942-12-05
File — Object: 66/84 - 66/115, Folder: Arch 66/96
Dates:
1942-12-05
Pressure distribution measurements on the A4 V1P in the area of the subsonic and supersonic speed ducts, 1942-11-29
File — Object: 66/84 - 66/115, Folder: Arch 66/100
Dates:
1942-11-29
The axial symmetric fow around the body of the missile A4 at Mach numbers 1.86 and 1.56, 1942-11-17
File — Object: 66/84 - 66/115, Folder: Arch 66/101
Dates:
1942-11-17
Spin torque measurements on the A4 V1P with enlarged air rudders DR IIf, 1942-11-10
File — Object: 66/84 - 66/115, Folder: Arch 66/103
Dates:
1942-11-10
Multi-component measurements on models of the Peenemünder Pfeil bullets PPG/T/10.5/2400/60/1/A and PPG/F/15/2500/87/1/A, 1943-04-13
File — Object: 66/84 - 66/115, Folder: Arch 66/104
Dates:
1943-04-13
Three component measurements on models of the Tap Bullet 52/38 and Tap-R Bullet 52/38, 1942-12-05
File — Object: 66/84 - 66/115, Folder: Arch 66/107 (Copy)
Dates:
1942-12-05
The adjustment of three-component measurements according to the method of least squares, 1943-05-12
File — Object: 66/84 - 66/115, Folder: Arch 66/109 (Copy)
Dates:
1943-05-12
Three component measurements on models of the Tap Bullet 80/52, the Tap-R Bullet 80/52 and the R Bullet 80 and 52, 1943-03-24
File — Object: 66/84 - 66/115, Folder: Arch 66/110 (Copy)
Dates:
1943-03-24
Pressure distribution measurements on a Drem flap BK5 of the A4V1P with a flap setting angle nK = 110 degrees at Ma = 2.47, 1943-03-07
File — Object: 66/84 - 66/115, Folder: Arch 66/111
Dates:
1943-03-07