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de Vries, Reynard
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1
Aerodynamic Performance Benefits of Over-the-Wing Distribut..:
de Vries, Reynard
;
Vos, Roelof
Journal of Aircraft. 60 (2023) 4 - p. 1201-1218 , 2023
Link:
https://doi.org/10.2514/..
?
2
Cross-Validation of Hybrid-Electric Aircraft Sizing Methods:
Finger, D. Felix
;
de Vries, Reynard
;
Vos, Roelof
..
Journal of Aircraft. 59 (2022) 3 - p. 742-760 , 2022
Link:
https://doi.org/10.2514/..
?
3
Aerodynamic Performance and Static Stability Characteristic..:
van Arnhem, Nando
;
de Vries, Reynard
;
Sinnige, Tomas
..
Journal of Aircraft. 59 (2022) 2 - p. 415-432 , 2022
Link:
https://doi.org/10.2514/..
?
4
Aerodynamic interaction between propellers of a distributed..:
de Vries, Reynard
;
van Arnhem, Nando
;
Sinnige, Tomas
..
Aerospace Science and Technology. 118 (2021) - p. 107009 , 2021
Link:
https://doi.org/10.1016/..
?
5
Range Equation for Hybrid-Electric Aircraft with Constant P..:
de Vries, Reynard
;
Hoogreef, Maurice F. M.
;
Vos, Roelof
Journal of Aircraft. 57 (2020) 3 - p. 552-557 , 2020
Link:
https://doi.org/10.2514/..
?
6
Preliminary Sizing Method for Hybrid-Electric Distributed-P..:
de Vries, Reynard
;
Brown, Malcom
;
Vos, Roelof
Journal of Aircraft. 56 (2019) 6 - p. 2172-2188 , 2019
Link:
https://doi.org/10.2514/..
?
7
Alleviation of Propeller-Slipstream-Induced Unsteady Pylon ..:
Sinnige, Tomas
;
Corte, Biagio Della
;
De Vries, Reynard
...
Journal of Aircraft. 56 (2019) 3 - p. 1214-1230 , 2019
Link:
https://doi.org/10.2514/..
?
8
Unsteady Pylon Loading Caused by Propeller-Slipstream Impin..:
Sinnige, Tomas
;
de Vries, Reynard
;
Corte, Biagio Della
...
Journal of Aircraft. 55 (2018) 4 - p. 1605-1618 , 2018
Link:
https://doi.org/10.2514/..
?
9
An Overview of the Conceptual Design Studies of Hybrid Elec..:
Zill, Thomas
;
Iwanizki, Michael
;
Schmollgruber, Peter
...
info:eu-repo/grantAgreement/EC/H2020/807097/. , 2020
Link:
https://zenodo.org/recor..
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