000 00456pam a2200157a 44500
082 _aTR
_bCOA-194
100 _aStevenson,T. N.
245 1 _aMODIFIED VELOCITY DEFECT LAW FOR TURBULENT BOUNDARY LAYERS WITH INJECTION
250 _a1967
260 _a
_bCollege Of Aeronautics, Cranfield
_c
300 _a10
440 _aCollege Of Aeronautics Report
_vNo,170
500 _aBound With: Coa Rep Aero No.170-199
964 _gCIRC
997 _aTR3003 C
999 _c392724
_d392724