000 00452pam a2200133a 44500
082 _aR&M-3768
100 _aEast, L.F.
245 1 _aMEASUREMENTS OF THE THREE DIMENSIONAL INCOMPRESSIBLE TURBULENT BOUNDARY LAYER INDUCED ON THE SURFACE OF A SLENDER DELTA WING BY THE...
260 _a
_b
_c
440 _aAeronautical Research Council Reports And Memoranda
_vR&M 3768
500 _aBound With:Arc R&M 3760-3768
964 _gCIRC
997 _aTR6201 C
999 _c392027
_d392027