Remarks on the structure of conical flow

Progress in Aerospace Sciences

Volumn 12, Issue C, 1972, Pages 241-272

  Smith, J H B ^a  

^a Royal Aircraft Establishment   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 49649140360     PISSN: 03760421     EISSN: None     Source Type: Journal    
DOI: 10.1016/0376-0421(72)90006-1     Document Type: Article

References (17)

1. The air pressure on a cone moving at high speeds
2. Aerodynamics of wings at high speeds
3. A method for designing lifting configurations for high supersonic speeds, using axisymmetric flow fields
4. The structure of concentrated vortex cores
5. The flow field near the centre of a rolled-up vortex sheet
6. An asymptotic solution for the centre of a rolled-up conical vortex sheet in compressible flow
7. Lignes de courant d'un écoulement continu
8. Vortex sheets rolling-up along leading edges
9. Supersonic flows with shock waves
10. A theory of the flow past a slender delta wing with leading-edge separation
11. The Flow Fields near the Centre of a Slender Rolled-up Conical Vortex Sheet
12. The compressible inviscid leading-edge vortex
13. Improved Calculations of Leading-edge Separation from Slender Delta Wings