Wind Tunnel Pressure Signatures for a 0.0041-Scale Model of the Space Shuttle Orbiter
Wind-Tunnel Investigation at a Mach Number of 1.53 of an Airplane with a Triangular Wing
Visualisation Study of the Vortex Flow Around Double-Delta Wings
Transonic Flutter Study of a 50.5 Deg Cropped-delta Wing with Two Rearward-Mounted Nacelles
The delta and Thor/ Agena Launch Vehicles for Scientific and Applications Satellites
The Behaviour of the Leading-Edge Vortices over a delta Wing Following a Sudden Change of Incidence
The Behaviour of the Leading-Edge Vortices over a delta Wing Following a Sudden Change of Incidence
Supersonic Flutter Derivatives for a Series of Swept and Cropped delta Wings
Sting Influence on Vortex Breakdown on a 65 Degree Delta Wing in Transonic Flow