The effects of Mach and Reynolds number on the flow mixing properties of micro-ramp vortex generators in a supersonic boundary layer

RHM Giepman; A Srivastava; FFJ Schrijer; BW van Oudheusden

doi:10.2514/6.2015-2779

The effects of Mach and Reynolds number on the flow mixing properties of micro-ramp vortex generators in a supersonic boundary layer

RHM Giepman, A Srivastava, FFJ Schrijer, BW van Oudheusden

Aerodynamics

Research output: Chapter in Book/Conference proceedings/Edited volume › Conference contribution › Scientific › peer-review

4 Citations (Scopus)

Original language	English
Title of host publication	Proceedings of the 45th AIAA fluid dynamics conference
Editors	s.n.
Place of Publication	Reston
Publisher	American Institute of Aeronautics and Astronautics Inc. (AIAA)
Pages	1-18
Number of pages	18
ISBN (Print)	978-1-62410-362-9
DOIs	https://doi.org/10.2514/6.2015-2779
Publication status	Published - 2015
Event	45th AIAA fluid dynamics conference, Dallas, USA - Reston Duration: 22 Jun 2015 → 26 Jun 2015

Publication series

Name
Publisher	AIAA

Conference

Conference	45th AIAA fluid dynamics conference, Dallas, USA
Period	22/06/15 → 26/06/15

Bibliographical note

harvest
AIAA 2015-2780

Access to Document

10.2514/6.2015-2779

Cite this

Giepman, RHM., Srivastava, A., Schrijer, FFJ., & van Oudheusden, BW. (2015). The effects of Mach and Reynolds number on the flow mixing properties of micro-ramp vortex generators in a supersonic boundary layer. In s.n. (Ed.), Proceedings of the 45th AIAA fluid dynamics conference (pp. 1-18). American Institute of Aeronautics and Astronautics Inc. (AIAA). https://doi.org/10.2514/6.2015-2779

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title = "The effects of Mach and Reynolds number on the flow mixing properties of micro-ramp vortex generators in a supersonic boundary layer",

author = "RHM Giepman and A Srivastava and FFJ Schrijer and {van Oudheusden}, BW",

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doi = "10.2514/6.2015-2779",

language = "English",

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Giepman, RHM, Srivastava, A, Schrijer, FFJ & van Oudheusden, BW 2015, The effects of Mach and Reynolds number on the flow mixing properties of micro-ramp vortex generators in a supersonic boundary layer. in s.n. (ed.), Proceedings of the 45th AIAA fluid dynamics conference. American Institute of Aeronautics and Astronautics Inc. (AIAA), Reston, pp. 1-18, 45th AIAA fluid dynamics conference, Dallas, USA, 22/06/15. https://doi.org/10.2514/6.2015-2779

The effects of Mach and Reynolds number on the flow mixing properties of micro-ramp vortex generators in a supersonic boundary layer. / Giepman, RHM; Srivastava, A; Schrijer, FFJ et al.
Proceedings of the 45th AIAA fluid dynamics conference. ed. / s.n. Reston: American Institute of Aeronautics and Astronautics Inc. (AIAA), 2015. p. 1-18.

Research output: Chapter in Book/Conference proceedings/Edited volume › Conference contribution › Scientific › peer-review

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T1 - The effects of Mach and Reynolds number on the flow mixing properties of micro-ramp vortex generators in a supersonic boundary layer

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AU - Schrijer, FFJ

AU - van Oudheusden, BW

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BT - Proceedings of the 45th AIAA fluid dynamics conference

A2 - s.n., null

PB - American Institute of Aeronautics and Astronautics Inc. (AIAA)

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T2 - 45th AIAA fluid dynamics conference, Dallas, USA

Y2 - 22 June 2015 through 26 June 2015

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Giepman RHM, Srivastava A, Schrijer FFJ , van Oudheusden BW. The effects of Mach and Reynolds number on the flow mixing properties of micro-ramp vortex generators in a supersonic boundary layer. In s.n., editor, Proceedings of the 45th AIAA fluid dynamics conference. Reston: American Institute of Aeronautics and Astronautics Inc. (AIAA). 2015. p. 1-18 doi: 10.2514/6.2015-2779