Box 19
Container
Contains 113 Results:
Nomogram for the drag coefficient cw as function of altitude h, velocity v, and angle of attack d., 1948-06
File — Box: 19, Folder: Arch 14/9
Dates:
1948-06
Analysis of reaction thrust, Optimum Thrust Curve for vertical motion of various missiles taking drag into consideration, 1948-06
File — Box: 19, Folder: Arch 14/10
Dates:
1948-06
Numerical data in addition to Arch 14/7 "Fundamental considerations regarding the equations of motion", 1948-02
File — Box: 19, Folder: Arch 14/11
Dates:
1948-02
Trajectory of a model missile acted upon by wind. Results of computation., 1946-04
File — Box: 19, Folder: Arch 14/12
Dates:
1946-04
Separation of Oscillations for the purpose of computing trajectories and testing stability, 1946-02
File — Box: 19, Folder: Arch 14/13
Dates:
1946-02
Damping Proportional to the variation of the missile angle effect on former reports, 1940-12-21
File — Box: 19, Folder: Arch 14/15
Dates:
1940-12-21
Numerical table of the air density ration, decrease of pressure, velocity of sound, and acceleration due to gravity as functions of the altitude, 1941-01-15
File — Box: 19, Folder: Arch 14/16
Dates:
1941-01-15
Numerical tables for determination of aerodynamic coefficients and the distance H/D of the center of Pressure referred to caliber, 1941-01-15
File — Box: 19, Folder: Arch 14/17
Dates:
1941-01-15
Measurement of the missile trajectory using electro-magnetic waves, 1957-04
File — Box: 19, Folder: HAP Arch 7/6-Trans
Dates:
1957-04