Searched for: author:"Meijer, J.J."
(1 - 14 of 14)
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Meijer, J.J. (author)
report 2013
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Meijer, J.J. (author)
report 2013
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Meijer, J.J. (author)
master thesis 2013
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Meijer, J.J. (author)
master thesis 2013
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Haringa, M.J. (author), Meijer, J.J. (author), Rijzebol, K.R. (author)
The Royal Netherlands Air Force has carried out an analysis and test program with the F-16A/B (Mid Life Update version) aircraft for the airworthiness certification of the Lockheed Martin Overseas Corporation "Enhanced Targeting Pod" and the British Aerospace Systems "Falcon Owl" navigation pod (earlier known as "Atlantic" Navigation pod)....
report 2001
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Meijer, J.J. (author)
doctoral thesis 1989
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Meijer, J.J. (author)
An outline is given of store flutter clearance activities of the NLR carried out by order of the Royal Netherlands Air Force. Special attention is devoted to the store flutter clearance of the F16 aircraft. Presented at: 7th Aircraft/Stores Compatibility Symposium,Wright-Patterson AFB, Ohio, 8-10 April 1986 and at the 17th Annual Symposium of...
report 1986
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Overwater, T. (author), Meijer, J.J. (author)
Document(en) uit de collectie Chemische Procestechnologie.
report 1984
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Hounjet, M.H.L. (author), Meijer, J.J. (author)
Unsteady aerodynamic loads in the transonic domain have been obtained with time-linearized methods in which a so-called field panel method is embedded which accounts for a proper radiation of signals towards infinity. The methods are used to predict the unsteady loads and first harmonic pressure distributions on an airfoil and a transport type...
report 1984
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Hounjet, M.H.L. (author), van der Kolk, J.T. (author), Meijer, J.J. (author)
unsteady and quasi-steady aerodynamic loads in the transonic flow domain have been obtained from NLR's numerical simulation methods for transonic potential flow. The unsteady results have been obtained with the time-linearized finite volume method FTRAN3, embedding a so-called field panel method which accounts for proper radiation of signals...
report 1984
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Persoon, A.J. (author), Horsten, J.J. (author), Meijer, J.J. (author)
Flutter experiments were performed on a supercritical transport-type wing with the aim to investigate the transonic dip in the flutter boundaries and to obtain data for verification of a calculation method for unsteady aerodynamic loads. Complete transonic dips were measured at three wing angles of attack. At the highest wing angle of attack...
report 1983
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Meijer, J.J. (author), Zwaan, R.J. (author)
Het onderzoek in het kader van onderwerp S4 is gericht op het verbeteren van theoretische en experimentele methoden voor flutter- en trillingsonderzoek. De werkzaamheden voor I98I hebben voornamelijk betrekking op het ontwikkelen van een methode waarmee bewegingsvergelijkingen voor het elastisch vervormende vliegtuig direct kunnen worden...
report 1981
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van Nunen, J.W.G. (author), Roos, R. (author), Meijer, J.J. (author)
A description and results are given of an extensive research program set up to determine the unsteady aerodynamic loading on oscillating wing-store configurations. It is shown that the tools developed in the course of the program allow for a more accurate prediction of the unsteady airforces introduced by wing mounted stores.
report 1977
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Meijer, J.J. (author), van der Neut, A. (author)
report 1970
Searched for: author:"Meijer, J.J."
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