1. 1-0 SUPERSONIC NOZZLE
2. 5- •1.5 -1.0 -0.5 0.0 O.S 1.0 I.S 2.0 2.5 3.0 3.5
3. This work was partially supported by NASA Ames Research Center under Contract NAS2-11920, by AFOSR under Contract F49620-83-C-0084 and by ARO under Contract DAAG29-84-C0002.