A THEORY FOR THE CORE OF A LEADING-EDGE VORTEX

[1] COX AP, 1959, 21116 AER RES COUN R

[2] EARNSHAW PB, 1961, 22876 AER RES COUN R

[3] ELLE BJ, 1958, 19780 AER RES COUN R

[4] HALL MG, 1960, 22660 AER RES COUN R

[5] HALL MG, 1959, 21117 AER RES COUN R

[6] JONES JP, 1960, USAA140 U SOUTH REP

[7] LAMBOURNE NC, 1959, 21073 AER RES COUN R

[8] A THEORY OF THE FLOW PAST A SLENDER DELTA WING WITH LEADING EDGE SEPARATION [J]. PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES, 1959, 251 (1265): : 200 - 217

[9] FLOW IN A VISCOUS TRAILING VORTEX [J]. AERONAUTICAL QUARTERLY, 1959, 10 (02): : 149 - 162

[10] PECKHAM DH, 1958, 20727 AER RES COUN R

[1] COX AP, 1959, 21116 AER RES COUN R

[2] EARNSHAW PB, 1961, 22876 AER RES COUN R

[3] ELLE BJ, 1958, 19780 AER RES COUN R

[4] HALL MG, 1960, 22660 AER RES COUN R

[5] HALL MG, 1959, 21117 AER RES COUN R

[6] JONES JP, 1960, USAA140 U SOUTH REP

[7] LAMBOURNE NC, 1959, 21073 AER RES COUN R

[8] A THEORY OF THE FLOW PAST A SLENDER DELTA WING WITH LEADING EDGE SEPARATION [J]. PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES, 1959, 251 (1265): : 200 - 217

[9] FLOW IN A VISCOUS TRAILING VORTEX [J]. AERONAUTICAL QUARTERLY, 1959, 10 (02): : 149 - 162

[10] PECKHAM DH, 1958, 20727 AER RES COUN R