Author

A.C. de Bruin

Observed names: A. C. Bruin, A. C. De Bruin, A. C. de Bruin, de Bruin, A.C.

Observed institution: Netherlands Aerospace Centre

OpenAlex ID: A5030304354

Flow field survey in trailing vortex system behind a civil aircraft model at high lift

1996 · A.C. de Bruin, G.H. Hegen, et al. · 24

S-Wake Assessment of Wake Vortex Safety

2003 · A.C. de Bruin · 19

Experimental pressure wave research at NLR for high-speed rail tunnels

1998 · E.A.F.A. Demmenie, A.C. de Bruin, et al. · 10

A Quantitative Analysis of Viscous and Lift-induced Drag Components from Detailed Wake Measurements behind a Half-Span Model

2002 · F.L.A. Ganzevles, A.C. de Bruin, et al. · 8

KAI Surion helicopter full-scale air intake testing at CIRA Icing Wind Tunnel

2016 · A.C. de Bruin, G. Fatigati, et al. · 5

A discussion of measured static and dynamic rotor loads during testing of the ERICA tilt-wing rotorcraft configuration in DNW-LLF wind tunnel

2014 · A.C. de Bruin, Oliver Schneider · elib (German Aerospace Center) · 4

Wake vortex results from the AWIATOR project

2007 · A.C. de Bruin, G. Schrauf · 4

The Effect of a Single Cylindrical Roughness Element on Boundary Layer Transition in a Favourable Pressure Gradient

1990 · A. C. de Bruin · Springer eBooks · 4

Wake vortex safety evaluation of single runway approaches under different weather and operational conditions

2002 · G. B. van Baren, L.J.P. Speijker, et al. · 3

Transition For Airfoils of GARTEUR AD (AG14)

1994 · D Arnal, A.C. de Bruin, et al. · elib (German Aerospace Center) · 2

Computation of three-dimensional boundary layer transition and separation on a 65deg swept delta wing at 20deg angle of attack

1986 · A.C. de Bruin, H.W.M. Hoeijmakers · 2

Turbulence modelling of the shear layers in the trailing edge region of a modern rear-loaded airfoil at incidence

1993 · A. C. Bruin, L. H. J. Absil, et al. · Flow Turbulence and Combustion · 1

Turbulence Modelling of the Shear Layers in the Trailing Edge Region of a Modern Rear-Loaded Airfoil at Incidence

1993 · A. C. De Bruin, L. H. J. Absil, et al. · Fluid mechanics and its applications · 1

A Method for Three-Dimensional Boundary Layer Calculations on Arbitrary Bodies: Some Results on Aircraft Wings and Engine Cowls

1982 · J. P. F. Lindhout, A. C. de Bruin, et al. · Springer eBooks · 1

Tracking dynamically scaled objects during a helicopter wind tunnel test

2018 · A.C. de Bruin, Karel Lammers, et al.

Rotor-wing interaction phenomena for the ERICA tilt-wing rotorcraft configuration in the DNW-LLF wind tunnel

2015 · A.C. de Bruin, Oliver Schneider · elib (German Aerospace Center)

Prospects for head- and crosswind dependent aircraft separations in the context of wake vortex safety and airport capacity

2005 · A.C. de Bruin

Wake vortex safety evaluation of single runway Wake vortex safety evaluation of single runway Wake vortex safety evaluation of single runway Wake vortex safety evaluation of single runway

2002 · G. B. van Baren, L.J.P. Speijker, et al.

New attempts to solve an old problem: Aerodynamic measurements in new vehicle tunnels

1997 · A.C. de Bruin, R.A. Maarsingh, et al.

Derivation of Linear Stability Equations in Orthogonal Curvi-Linear Coordinates, Using a Formula Manipulation Program

1992 · A.C. de Bruin

Experiments and Theoretical Considerations Regarding the Allowable Surface Roughness Height in Laminar Flow

1992 · A.C. de Bruin

Boundary layer calculations on the leeward surface of a slender delta wing at incidence

1983 · A.C. de Bruin

Works count: 25

Citation count: 88

H-index: 5

I10-index: 3