HIGHER-ORDER BOUNDARY-LAYER THEORY

[71] NONWEILER T, 1952, 62 COLL AER CRANF EN

[72] OBERAI MM, 1964, J MECANIQUE, V3, P175

[73] OVCHINNIKOV ON, 1960, SOV PHYS-TECH PHYS, V5, P590

[74] PAN LJ, 1956, J MATH PHYS, V35, P179

[75] PEARSON JRA, 1957, THESIS U CAMBRIDGE

[76] PRANDTL L, 1935, AERODYNAMIC THEORY, V3, P34

[77] Rosenhead L., 1963, LAMINAR BOUNDARY LAY

[78] THE EFFECT OF SLIP, PARTICULARLY FOR HIGHLY COOLED WALLS [J]. JOURNAL OF THE AEROSPACE SCIENCES, 1962, 29 (05): : 591 - 595

[79] VORTICITY EFFECT ON THE STAGNATION-POINT FLOW OF A VISCOUS INCOMPRESSIBLE FLUID [J]. JOURNAL OF THE AEROSPACE SCIENCES, 1959, 26 (08): : 542 - 543

[80] INCOMPRESSIBLE FLOW ALONG A CORNER [J]. JOURNAL OF FLUID MECHANICS, 1966, 26 : 97 - &

[71] NONWEILER T, 1952, 62 COLL AER CRANF EN

[72] OBERAI MM, 1964, J MECANIQUE, V3, P175

[73] OVCHINNIKOV ON, 1960, SOV PHYS-TECH PHYS, V5, P590

[74] PAN LJ, 1956, J MATH PHYS, V35, P179

[75] PEARSON JRA, 1957, THESIS U CAMBRIDGE

[76] PRANDTL L, 1935, AERODYNAMIC THEORY, V3, P34

[77] Rosenhead L., 1963, LAMINAR BOUNDARY LAY

[78] THE EFFECT OF SLIP, PARTICULARLY FOR HIGHLY COOLED WALLS [J]. JOURNAL OF THE AEROSPACE SCIENCES, 1962, 29 (05): : 591 - 595

[79] VORTICITY EFFECT ON THE STAGNATION-POINT FLOW OF A VISCOUS INCOMPRESSIBLE FLUID [J]. JOURNAL OF THE AEROSPACE SCIENCES, 1959, 26 (08): : 542 - 543

[80] INCOMPRESSIBLE FLOW ALONG A CORNER [J]. JOURNAL OF FLUID MECHANICS, 1966, 26 : 97 - &