B. Gothert

• Aerofoil measurements in the DVL (2.7M) high-speed wind tunnel
• Calculation of the velocity field of sweptback wings at high subsonic speeds
• High speed tests on symmetrical profiles with different thickness ratios in the DVL high-speed wind tunnel (2.7m. dia.) and comparison with measurements in other wind tunnels
• Pressure distribution and momentum loss diagram for the NACA profile 0 00 12- 1.1 30 at high subsonic speed
• Pressure distribution and momentum loss diagrams for the NACA profile 0 00 09-1.1 30 at high subsonic speed
• Pressure distribution and momentum loss diagrams for the NACA profile 0 00 18 - 1.1 30 at high subsonic speed
• Two- and three-dimensional flow at high subsonic speeds: extension of the Prandtl rule