1956•NASA STI Repository (National Aeronautics and Space Administration)Requires access
Transonic-wind-tunnel Investigation of the Effects of Lip Bluntness and Shape on the Drag and Pressure Recovery of a Normal-shock Nose Inlet in a Body of Revolution
W. B. Olstad
Open publisher page 3 citations
Abstract
This record does not include an abstract. Use the full-text link above if available.