An Estimate of the Installed Drag Co-efficient of Wing Mounted Stores for the Mach Number Range 0.8 to 2.0
1955 Oct 17
Originating Research Org.:
Sandia National Lab. (SNL-NM), Albuquerque, NM (United States)
OpenNet Entry 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.