Issue Section:
Discussions
1.
Dong
Y.
Cumpsty
N. A.
1990
, “Compressor Blade Boundary Layers: Part I—Test Facility and Measurements With No Incident Wakes; Part II—Measurements With Incident Wakes
,” ASME JOURNAL OF TURBOMACHINERY
, Vol. 112
, pp. 222
–240
.2.
Hodson, H. P., 1991, “Aspects of Unsteady Blade-Surface Boundary Layers and Transition in Axial Turbomachines,” in: VKI Lecture Series No. 9, Boundary Layers in Turbomachines, Von Karman Institute.
3.
Hodson
H. P.
Addison
J. S.
Shepherdson
C. A.
1992
, “Models for Unsteady Wake-Induced Transition in Axial Turbomachines
,” Jnl. de Physique
, Vol. 2
, No. 4
, Apr., pp. 545
–574
.4.
Hodson
H. P.
Huntsman
I.
Steele
A. B.
1994
, “An Investigation of Boundary Layer Development in a Multistage LP Turbine
,” ASME JOURNAL OF TURBOMACHINERY
, Vol. 116
, pp. 375
–383
.
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