1. Boundary layer simulation and control in wind tunnels;AGARD Fluid Dynamics Panel;AGARD AR 224,1987
2. The importance of high Reynolds number in low-speed wind tunnel tests of canard delta combat aircraft;Peckham;RAE Technical Memorandum Aero,1987
3. Scale effects in transonic flow;Haines,1987
4. Reynolds number effects in transonic flow;Elsenaar;AGARD AG 303,1988
5. The air-injection method of fixing boundary-layer transition and investigating scale effects;Ashill;Aeronautical J. R. Aeronautical Soc.,1987