Document Details

An Estimate of the Installed Drag Co-efficient of Wing Mounted Stores for the Mach Number Range 0.8 to 2.0
Document Type:
Publication Date:
1955 Oct 17
Document Pages:
27 p.
Document Number(s):
SC-TM-173-55(51); ALSNL199700000639
Originating Research Org.:
Sandia National Lab. (SNL-NM), Albuquerque, NM (United States)
OpenNet Entry Date:
1999 Sep 28
OpenNet Modified Date:
1999 Sep 28
This was in relationship to interceptor-type airplanes. The data was derived from wind-tunnel and free-flight tests, conducted primarily by the NACA. The important numbers were analyzed at transonic and supersonic Mach numbers.

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