Experimental study of the flow over a particular afterbody shape having a near-sonic ridge line

von Treadgold, D.
Veröffentlicht 1961

Aerodynamic characteristics at M : = 4.3 of monoplane, triform and cruciform slender delta wing bodies with all-moving tail control surfaces

von Treadgold, D.
Veröffentlicht 1968

Some examples of the use of a conical shadowgraph technique

von Pierce, D.
Veröffentlicht 1964

Tests at M=2.47

von Watts, P. E.
Veröffentlicht in A wind tunnel investigation of the longitudinal and lateral aerodynamic characteristics of a canard aircraft model (1962)

Some examples of the application of methods for the prediction of boundary-layer transition of sheared wings

von Treadgold, D. A.
Veröffentlicht 1973

Force and moment measurements on a conical body and a rectangular wing, separately and in combination,at Mach number 1.94

von Anderson, J. R.
Veröffentlicht 1956

A wind tunnel investigation of the longitudinal and lateral aerodynamic characteristics of a canard aircraft model

Veröffentlicht 19591962