Wind-Tunnel Tests of the Navy Low-Drag Bomb at Angles of Attack up to 70 Degrees
NAVAL ORDNANCE LAB WHITE OAK MD
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The report presents the results of an investigation in the NOL supersonic tunnel to measure the static stability and drag of the Navy low-drag bomb at angles of attack up to 70 degrees. These data were obtained at Mach numbers of 0.40, 0.60, 0.80, 1.53, 1.76, and 2.03.
- Aerial Bombs