NPOC - SPOT enquête 1986

Uitbreiding van het NLR computernetwerk met een supercomputer

Globale evaluatie van het tipvaan concept m.b.v. een dragende-lijn model

Comment on the yaw stability of a horizontal-axis wind turbine at small angles of yaw

General introduction to wind energy conversion

Second series of wind-tunnel tests on a model of two-bladed horizontal-axis wind turbine; influence of turbulence on the turbine performance and results of a aflow survey behind the rotor

Wind-tunnel tests on a model of a two-bladed horizontal-axis wind turbine and evaluation of an aerodynamic performance calculation method

The aerodynamic performance of a horizontal-axis wind turbine in a stationary parallel flow: Discussion of existing theories, of a parameter study and of consequences for a wind tunnel model design

Rigid rotor computer program for the Darrieus wind turbine: Performance and blade loading

Contribution of NLR to the first phase of the National Research Progam on wind energy. Part I: Rigid rotor computer program and preparatory work for a test-bed

Two-dimensional tunnel wall interference for multi-element aerofoils in incompressible flow

Aerodynamische aspecten windgedreven rotoren; enige orienterende beschouwingen

Evaluation of a potential theoretical model of the wake behind a wing via comparison of measurements and calculations

The deformation of a vortex sheet behind a swept back wing; comparison of measurements and calculations

Windtunnel investigation of the development of the vortex wake behind a sweptback wing: part I: text and tables

Windtunnel investigation of the development of the vortex wake behind a sweptback wing: part II: figures

Comments on the methods developed at NLR for conducting two-dimensinal research on high-lift devices.

Evaluation of a method for the calculation of the pressure distribution on two-dimensional wing-flap configurations in subsonic flow (part II)

Evaluation of a method for the calculation of the pressure distribution on two-dimensional wing-flap configurations in subsonic flow (part I)

Potential flow calculations to support two-dimensional wind tunnel tests on high-lift devices