Inverse relations
[ .. ] → schema:author → Elsenaar, A.
A break-down of sting interference effects / by A. Elsenaar and S.O.T.H. Hanschema:ProductModel
A survey on Schiphol Airport of the contamination of wing leading edges of three different aircraft types under operating conditions / by A. Elsenaar and H.N. Haasnootschema:ProductModel
An experimental study of the flow over a sharp-edged delta wing at subsonic and transonic speeds / by A. Elsenaar and H.W.M. Hoeijmakersschema:ProductModel
Experimental study on vortex and shock wave development on a 65° delta wing / by A. Elsenaar and K.A. Bütefischschema:ProductModel
Observed Reynolds number effects on airfoils and high aspect ratio wings at transonic flow conditions / by A. Elsenaarschema:ProductModel
On Reynolds number effects and simulation : report of the review committee of Agard working group 09 / by A. Elsenaarschema:ProductModel
Reynolds number effects and the wind tunnnel environment / by A. Elsenaarschema:ProductModel
Separation in transonic flow : a shocking experience / by A. Elsenaarschema:ProductModel
The international vortex flow experiment : a test case for compressible Euler codes / by A. Elsenaarschema:ProductModel
The modernization program of the transonic windtunnel HST of NLR : lessons from the past, prospects for the future / by A. Elsenaar and F. Jaarsmaschema:ProductModel
The windtunnel as a tool for laminar flow research / by A. Elsenaarschema:ProductModel
Vortex formation and flow separation: the beauty and the beast in aerodynamics : Lanchester 2000 lecture / A. Elsenaarschema:ProductModel
[ .. ] → schema:contributor → Elsenaar, A.
Comparison of boundary layer calculations for the root section of a wing : The September 1979 Amsterdam Workshop test case / by J.P.F. Lindhout, B. van den Berg and A. Elsenaarschema:ProductModel
Evaluation of an experimental technique to investigate the effects of the engine position on engine/pylon/wing interference / by J.A.J. van Engelen, B. Munniksma and A. Elsenaarschema:ProductModel
Half-model testing in the NLR high speed tunnel HST: its technique and application / by S.J. Boersen and A. Elsenaarschema:ProductModel
Instrumentation requirements for laminar flow research in the NLR high speed wind tunnel HST / by A. Elsenaar ... [et al.]schema:ProductModel
Tests on the AFWAL 65° delta wing at NLR : a study of vertex flow development between Mach = 0.4 and 4 / by S.J. Boersen and A. Elsenaarschema:ProductModel
The international vortex flow experiment / by A. Elsenaar ... [et al.]schema:ProductModel
The phase 2 up-grade of the NLR high speed tunnel HST / by F. Jaarsma and A. Elsenaarschema:ProductModel
Transonic aerodynamic efficiency assessment of an optimised supersonic civil transport using CFD / J. van Muijden and A. Elsenaarschema:ProductModel