Transonic Flight Tests to Determine Zero-Lift Drag and Pressure Recovery of Nacelles Located at the Wing Tips on a 45 Degree Sweptback Wing and Body Combination
Description:
Report presenting the zero-lift drag of a sweptback wing and body combination with nacelles with NACA 1-50-250 nose inlets locate in the wing tips as determined by flight tests of rocket-powered models at transonic speeds. Results regarding the pressure recovery and the effect of the nacelles on it are also provided.
Date:
January 11, 1952
Creator:
Hoffman, Sherwood & Pepper, William B., Jr.
Item Type:
Refine your search to only
Report
Partner:
UNT Libraries Government Documents Department