Accession Number:

AD0884854

Title:

Wind-Tunnel Tests of the Navy Low-Drag Bomb at Angles of Attack up to 70 Degrees

Descriptive Note:

Corporate Author:

NAVAL ORDNANCE LAB WHITE OAK MD

Report Date:

1960-10-04

Pagination or Media Count:

47.0

Abstract:

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.

Subject Categories:

  • Aerodynamics
  • Aerial Bombs

Distribution Statement:

APPROVED FOR PUBLIC RELEASE