The STOL aircraft wing application of Circulation Control was further investigated by Engler1a#39; at NSDRC. ... Consequently the cavity required to store the CC blowing tube for high speed cruise could not be accomodated inside the existing wing ... The very high temperature and pressure of the A6A jet engine bleed air required the use of titanium, see Figure 12. ... and _ ejector nozzle momentum ^ PVa2C The theoretical blowing coefficient agumentation is offset by the effects of internalanbsp;...
|Title||:||AIAA 83-0003 - AIAA 83-0094|