HISTORY OF BOUNDARY-LAYER THEORY

[1] ACKERET J, 1925, Z FLUGTECHN MOTORLUF, V16, P44

[2] ACKERET J, 1946, 10 I AER ZUR MITT

[3] ACKERET L, 1926, Z VEREINES DEUTSCHER, V70, P1153

[4] Bassett AB., 1888, TREATISE HYDRODYNAMI

[5] NOTE ON FREE TURBULENT FLOWS, WITH SPECIAL REFERENCE TO THE 2-DIMENSIONAL WAKE [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1950, 17 (07): : 441 - 445

[6] ON STEADY LAMINAR FLOW WITH CLOSED STREAMLINES AT LARGE REYNOLDS NUMBER [J]. JOURNAL OF FLUID MECHANICS, 1956, 1 (02) : 177 - 190

[7] RESULTS OF RECENT HYPERSONIC AND UNSTEADY FLOW RESEARCH AT THE LANGLEY-AERONAUTICAL-LABORATORY [J]. JOURNAL OF APPLIED PHYSICS, 1950, 21 (07) : 619 - 628

[8] BENNETT HW, 1953, REP KIMBERLY CLARK C

[9] FINITE AMPLITUDE EFFECTS IN AN UNSTABLE LAMINAR BOUNDARY LAYER [J]. PHYSICS OF FLUIDS, 1964, 7 (03) : 319 - 326

[10] A NON-LINEAR THEORY FOR OSCILLATIONS IN A PARALLEL FLOW [J]. JOURNAL OF FLUID MECHANICS, 1961, 10 (02) : 209 - 236

[1] ACKERET J, 1925, Z FLUGTECHN MOTORLUF, V16, P44

[2] ACKERET J, 1946, 10 I AER ZUR MITT

[3] ACKERET L, 1926, Z VEREINES DEUTSCHER, V70, P1153

[4] Bassett AB., 1888, TREATISE HYDRODYNAMI

[5] NOTE ON FREE TURBULENT FLOWS, WITH SPECIAL REFERENCE TO THE 2-DIMENSIONAL WAKE [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1950, 17 (07): : 441 - 445

[6] ON STEADY LAMINAR FLOW WITH CLOSED STREAMLINES AT LARGE REYNOLDS NUMBER [J]. JOURNAL OF FLUID MECHANICS, 1956, 1 (02) : 177 - 190

[7] RESULTS OF RECENT HYPERSONIC AND UNSTEADY FLOW RESEARCH AT THE LANGLEY-AERONAUTICAL-LABORATORY [J]. JOURNAL OF APPLIED PHYSICS, 1950, 21 (07) : 619 - 628

[8] BENNETT HW, 1953, REP KIMBERLY CLARK C

[9] FINITE AMPLITUDE EFFECTS IN AN UNSTABLE LAMINAR BOUNDARY LAYER [J]. PHYSICS OF FLUIDS, 1964, 7 (03) : 319 - 326

[10] A NON-LINEAR THEORY FOR OSCILLATIONS IN A PARALLEL FLOW [J]. JOURNAL OF FLUID MECHANICS, 1961, 10 (02) : 209 - 236