共 14 条
- [11] ROY M, 1957, RECHERCHE AERONAUTIQ, P3
- [12] IMPROVED CALCULATIONS OF LEADING-EDGE SEPARATION FROM SLENDER THIN DELTA WINGS [J]. PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES, 1968, 306 (1484): : 67 - &
- [13] TING L, 1971, AIRCRAFT WAKE TURBUL, P11
- [14] Widnall S. E., 1971, AIRCRAFT WAKE TURBUL, P305