----------------- FILE NUMBER 1----------------- AFOSR-STANFORD LIBRARY OF EVALUATED TURBULENCE DATA - INDEX TO THE TAPE CASE NUMBER NUMBER OF FILES FILE NUMBER TITLE 1 TABLE OF CONTENTS 0111 28 2 - 29 PO, J.K., LUND, E.G., &  GESSNER, F.B.; DEVELOPING FLOW IN A SQUARE DUCT. (SECONDARY FLOW OF THE SECOND KIND) 0112 4 30 - 33 HINZE, J.O.; SECONDARY CURRENTS IN THE TURBULENT FLOW THROUGH A STRAIGHT CONDUIT. 0141 30 34 - 63 SAMUEL, A.E. & JOUBERT, P.N.; INCREASINGLY ADVERSE PRESSURE GRADIENT FLOW. 0142 & 0143 39 64 - 102 POZZORINI, R.; SIX-DEGREE CONICAL DIFFUSER FLOW, LOW AND HIGH CORE TURBULENCE. 0211 2 103 - 104 BRADSHAW, P., HANCOCK, P.E.; EFFECT OF FREE STREAM TURBULENCE. 0231 & 0232 26 105 - 130 HOFFMANN, P.H. & BRADSHAW, P.; TURBULENT BOUNDARY LAYERS ON SURFACES OF MILD LONGITUDINAL CURVATURE. 0233 26 131 - 156 GILLIS, J.C., JOHNSTON, J.P.; TURBULENT BOUNDARY LAYER ON A CONVEX, CURVED SURFACE. 0234 17 157 - 173 HUNT, I.A. & JOUBERT, P.N.; EFFECTS OF SMALL STREAMLINE CURVATURE ON TURBULENT DUCT FLOW. 0235 17 174 - 190 SMITS, A.J., YOUNG, S.T.B. & BRADSHAW, P.; THE EFFECTS OF SHORT REGIONS OF HIGH SURFACE CURVATURE ON TURBULENT BOUNDARY LAYERS. (CONVEX 30 DEGREES) 0241 11 191 - 201 ANDERSEN, P.S., KAYS, W.M. & MOFFAT, R.J.; ZERO PRESSURE GRADIENT CONSTANT INJECTION. 0242 13 202 - 214 ANDERSEN, P.S., KAYS, W.M. & MOFFAT, R.J.; ADVERSE PRESSURE GRADIENT WITH CONSTANT SUCTION. 0244 11 215 - 225 FAVRE, A., DUMAS, R., VEROLLET, E. AND COANTIC, M.; ZERO PRESSURE GRADIENT WITH CONSTANT SUCTION. 0251 20 226 - 245 NLR INFINITE SWEPT WING EXPERIMENT. 0252 22 246 - 267 PART-ROTATING CYLINDER EXPERIMENT. (BISSONNETTE & MELLOR) 0253 26 268 - 293 CYLINDER ON A FLAT TEST PLATE. (DECHOW & FELSCH) 0254 23 294 - 316 PART-ROTATING CYLINDER. (LOHMANN) 0261, 0263, 0264 17 317 - 333 TURBULENT WALL JET DATA COLLECTED FROM VARIOUS SOURCES. 0311 6 334 - 339 PLANAR MIXING LAYER DEVELOPING FROM TURBULENT WALL BOUNDARY LAYERS. 0331 36 340 - 375 CASTRO, I.P. & BRADSHAW, P.; THE TURBULENCE STRUCTURE OF A HIGHLY CURVED MIXING LAYER. 0361 72 376 - 447 CHEVRAY, R.; THE TURBULENT WAKE OF A BODY OF REVOLUTION. 0370 (0371, 19 448 - 466 HOMOGENOUS TURBULENT FLOWS. 0372, 0373, 0374, 0375, 0376) 0381 & 0382 52 467 - 518 ANDREOPOULOS, J. & BRADSHAW, P.; MEASUREMENTS OF INTERACTING TURBULENT SHEAR LAYERS IN THE NEAR WAKE OF AN AIRFOIL. 0411 19 519 - 537 CANTWELL, B.J. & COLES, D.; A FLYING HOT WIRE STUDY OF THE TURBULENT NEAR WAKE OF A CIRCULAR CYLINDER AT A REYNOLDS NUMBER OF 140000. 0421 32 538 - 569 KIM, J., KLINE, S.J. & JOHNSTON, J.P.; FLOW OVER A BACKWARD FACING STEP. 0431 36 570 - 605 CHEW, Y.T., SIMPSON, R.L. & SHIVAPRASAD, B.G.; SEPARATING ADVERSE PRESSURE GRADIENT FLOW. 0441 4 606 - 609 WADCOCK, A.J. & COLES, D.E.; FLYING-HOT WIRE STUDY OF TWO-DIMENSIONAL TURBULENT SEPARATION OF AN NACA 4412 AIRFOIL AT MAXIMUM LIFT. 0471 48 610 - 657 VISWANATH, P.R., CLEARY, T.W., SEEGMILLER, H.L. & HORSTMAN, C.C.; TRAILING-EDGE FLOWS AT HIGH REYNOLDS NUMBER. 0511 135 658 - 792 SHABAKA, I.M.M.A; TURBULENT FLOW IN AN IDEALIZED WING-BODY JUNCTION. 0512 21 793 - 813 HUMPHREY, J.A.C.; TURBULENT FLOW IN A CURVED DUCT OF SQUARE CROSS-SECTION. 0612 25 814 - 838 WIEGHARDT, K.; ON THE TURBULENT FRICTION LAYER FOR RISING PRESSURE. 8301 3 839 - 841 THOMAS, G.D.; FAVORABLE PRESSURE GRADIENT AT SUPERSONIC SPEEDS WITH INJECTION. 8401 4 842 - 845 PEAKE, D.J., BRAKMANN, G. & ROMESKIE, J.M.; BOUNDARY LAYER IN ADVERSE PRESSURE GRADIENT. 8402 9 846 - 854 LEWIS, J.E., GRAN, R.L. & KUBOTA, T.; BOUNDARY LAYER IN ADVERSE PRESSURE GRADIENT. 8403 47 855 - 901 KUSSOY, M.I., HORSTMAN, C.C. & ACHARYA, M.; PRESSURE GRADIENT AND REYNOLDS NUMBER EFFECTS ON COMPRESSIBLE TURBULENT BOUNDARY LAYERS IN SUPER- SONIC FLOW. 8411 8 902 - 909 ZWARTS, F.J.; BOUNDARY LAYER IN ADVERSE PRESSURE GRADIENT. 8501 2 910 - 911 COMPRESSIBILITY EFFECTS ON FREE SHEAR LAYERS. (BRADSHAW) 8601 31 912 - 942 MATEER, G.C., BOSH, A. & VIEGAS, J.; NORMAL SHOCK-WAVE/TURBULENT BOUNDARY-LAYER INTERACTION AT TRANSONIC SPEEDS. 8602 119 943 - 1061 KOOI, J.W.; INFLUENCE OF FREE STREAM MACH NUMBER ON TRANSONIC SHOCK-WAVE BOUNDARY LAYER INTERACTION. 8611 14 1062 - 1075 BACHALO, W.D. & JOHNSON,D.A.; TRANSONIC TURBULENT BOUNDARY LAYER SEPARATION ON AN AXISYMMETRIC BUMP. 8612 44 1076 - 1119 DELERY, J. & LE DUIZET; TRANSONIC FLOW OVER 2-DIMENSIONAL BUMP, M = 1.37. 8621 74 1120 - 1193 COOK, P.H., MCDONALD, M.A. & FIRMIN, M.C.P.; AEROFOIL RAE 2822 - PRESSURE DISTRIBUTION AND BOUNDARY LAYER AND WAKE MEASUREMENTS. 8623 48 1194 - 1241 SPAID, F.W. & STIVERS, L.S.; SUPERCRITICAL AIRFOIL BOUNDARY LAYER MEASUREMENTS. 8631 50 1242 - 1291 SETTLES, G.S., FITZPATRICK, T.J. & BOGDONOFF, S.M.; ATTACHED AND SEPARATED COMPRESSION CORNER FLOW FIELDS IN HIGH REYNOLDS NUMBER SUPERSONIC FLOW. 8632 32 1292 - 1323 DUSSAUGE, J. & GAVIGLIO, J.; TURBULENT BOUNDARY-LAYER /EXPANSION INTERACTION AT SUPERSONIC SPEED. 8641 13 1324 - 1336 SETTLES, G.S., BACA, B.K., WILLIAMS, D.R. & BOGDONOFF, S.M.; REATTACHING PLANAR FREE SHEAR LAYER. (SUPERSONIC) 8651 34 1337 - 1370 HORSTMAN, C.C. & KUSSOY, M.I.; HYPERSONIC SHOCK WAVE TURBULENT BOUNDARY LAYER INTERACTION-WITH AND WITHOUT SEPARATION. 8661 7 1371 - 1377 PEAKE, D.J.; THREE DIMENSIONAL SWEPT SHOCK/TURBULENT BOUNDARY LAYER INTERACTION. 8663 47 1378 - 1424 KUSSOY, M.I., VIEGAS, J.R. & HORSTMAN, C.C.; INVESTIGATION OF 3-D SHOCK SEPARATED TURBULENT BOUNDARY LAYER. 8671 30 1425 - 1454 POINTED AXISYMMETRIC BODIES AT ANGLE OF ATTACK -SUPERSONIC. (RAINBIRD) 8691 13 1455 - 1467 MCDEVITT, J.B., SEEGMILLER, H.L. & OKUNO, H.L.; NON-LIFTING TRANSONIC AIRFOIL, SHOCK-SEPARATED FLOW. -------------- END OF FILE NUMBER 1------------- , SHOCK-SEPARATED