Pressure distribution and boundary layer investigations on 44 degree swept-back tapered wing part 1 three-dimensional tests on the wing part 2 two-dimensional pressure distribution tests on 10 per cent thick symmetrical aerofoil section
JavaScript is disabled for your browser. Some features of this site may not work without it.
Pressure distribution and boundary layer investigations on 44 degree swept-back tapered wing part 1 three-dimensional tests on the wing part 2 two-dimensional pressure distribution tests on 10 per cent thick symmetrical aerofoil section
