B. Van den Berg

发表

Windtunnel investigation on the effect of blowing over the flap and over the wing nose at various aspect ratios sweep angles and flap spans

B. Van den Berg, 1965 .

Windtunnel investigation with a two-dimensional airfoil on the effect of blowing over a flap and over a control surface

B. Van den Berg, 1962 .

On the role of laminar separation bubbles in airfoil leading edge stalls

B. Van den Berg, B. Berg, 1980 .

Technical evaluation report on the fluid dynamics panel symposium on improvement of aerodynamic performance through boundary layer control and high lift systems

B. Van den Berg, B. Oskam, 1985 .

Design of an airfoil leading edge slat using an inverse aerodynamic calculations method

B. Van den Berg, J. A. Van Egmond, 1984 .

Boundary layer measurements on a two-dimensional wing with flap and a comparison with calculations

B. Van den Berg, B. Oskam, 1979 .

Reynolds number and Mach number effects on the maximum lift and the stalling characteristicsof wings at low speeds

B. Van den Berg, B. Berg, 1969 .

Boudary layer measurements on a two-dimensional wing with flap

B. Van den Berg, B. Berg, 1979 .

A three-dimensional law of the wall for turbulent shear flows

B. Van den Berg, B. Berg, 1974, Journal of Fluid Mechanics.

Measurements in a three-dimensional incompressible turbulent boundary layer in an adverse pressure gradient under infinite swept wing conditions

A. Elsenaar, B. Van den Berg, A. Elsenaar, 1972 .