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Comparison of Drop and Wind-Tunnel Experiments on Bomb Drag at High Subsonic Speeds
The drag coefficients of bombs at high velocities velocity of fall was 97 percent of the speed of sound) (the highest are determined by drop tests and compared with measurements taken in the DVL high-speed closed wind tunnel and the open jet at AVA - Gottingen.
Date:
May 1948
Creator:
Göthert, B.
System:
The UNT Digital Library
Test Report on Three- and Six-Component Measurements on a Series of Tapered Wings of Small Aspect Ratio (Partial Report: Triangular Wing)
The investigations of the reports to 4 on wings of small aspect ratio are continued. The present report deals with the results of the three- and six-component measurements and the flow pictures of the triangular wing series with the aspect ratio Lambda = 3 to Lambda = 1.
Date:
May 1948
Creator:
Lange & Wacke
System:
The UNT Digital Library