TY  - CONF

T1  - Numerical prediction of the aerodynamic response of aerofoils subject to step increases in Mach number

JO  - Proceedings of the 23nd European Rotorcraft Forum

PY  - 1997/09/01

AU  - Shaw ST

AU  - Qin N

ED  - 

PB  - DGLR

VL  - 1

SP  - 31.1

EP  - 31.9

Y2  - 2024/12/27

ER  -