1953•NASA STI Repository (National Aeronautics and Space Administration)Requires access
Investigation at Transonic Speeds of Aerodynamic Characteristics of a Semielliptical Air Inlet in the Root of a 45 Degree Sweptback Wing
R. R. Howell, C. D. Trescot
Open publisher page 0 citations
Abstract
Report presenting an investigation in the transonic blowdown tunnel at Mach numbers from 0.63 to 1.41 to determine increments in lift, drag, and pitching moment of a sweptback semicircular air inlet installed in the root of a 45 degree sweptback wing. Results regarding internal pressures and inlet performances are provided.