Base pressure studies from over expanded nozzle for area ratio 2.56

by Baig, Maughal Ahmed Al, Khan, Sher Afghan, Rathakrishnan, E.
Published 2012

Control of suddenly expanded flows from correctly expanded and under expanded nozzles at supersonic mach number for area ratio 2.56

by Bashir, Musavir, Baig, Maughal Ahmed Al, Ismail, Ahmad Faris, Khan, Sher Afghan
Published 2016