Flow field characterization around test objects in a supersonic flow

R. A.L. Tolboom; A. P. van Vliett; N. M. Sijtsema; N. J. Dam; J. J. ter Meulen

doi:10.2514/6.2001-702

Flow field characterization around test objects in a supersonic flow

R. A.L. Tolboom, A. P. van Vliett, N. M. Sijtsema, N. J. Dam, J. J. ter Meulen

Research output: Contribution to conference › Paper › Academic

1 Citation (Scopus)

Abstract

Two dimensional Raman scattering images of the density field in a supersonic dry air flow around a sharp-edged wedge are presented. The images are used to characterize the flow field in terms of density, Mach number and angle of attack. Density ratios are determined both from geometrical features (shock angles) as well as directly from the Raman intensity distribution, yielding consistent results.

Original language	English
DOIs	https://doi.org/10.2514/6.2001-702
Publication status	Published - 2001
Externally published	Yes
Event	39th Aerospace Sciences Meeting and Exhibit 2001 - Reno, NV, United States Duration: 8-Jan-2001 → 11-Jan-2001

Conference

Conference	39th Aerospace Sciences Meeting and Exhibit 2001
Country/Territory	United States
City	Reno, NV
Period	08/01/2001 → 11/01/2001

Access to Document

10.2514/6.2001-702

Handle.net

Persistent link

Cite this

@conference{3bf847141bab464d96f8c5d87d04a9ec,

title = "Flow field characterization around test objects in a supersonic flow",

abstract = "Two dimensional Raman scattering images of the density field in a supersonic dry air flow around a sharp-edged wedge are presented. The images are used to characterize the flow field in terms of density, Mach number and angle of attack. Density ratios are determined both from geometrical features (shock angles) as well as directly from the Raman intensity distribution, yielding consistent results.",

author = "Tolboom, {R. A.L.} and {van Vliett}, {A. P.} and Sijtsema, {N. M.} and Dam, {N. J.} and {ter Meulen}, {J. J.}",

year = "2001",

doi = "10.2514/6.2001-702",

language = "English",

note = "39th Aerospace Sciences Meeting and Exhibit 2001 ; Conference date: 08-01-2001 Through 11-01-2001",

}

TY - CONF

T1 - Flow field characterization around test objects in a supersonic flow

AU - Tolboom, R. A.L.

AU - van Vliett, A. P.

AU - Sijtsema, N. M.

AU - Dam, N. J.

AU - ter Meulen, J. J.

PY - 2001

Y1 - 2001

N2 - Two dimensional Raman scattering images of the density field in a supersonic dry air flow around a sharp-edged wedge are presented. The images are used to characterize the flow field in terms of density, Mach number and angle of attack. Density ratios are determined both from geometrical features (shock angles) as well as directly from the Raman intensity distribution, yielding consistent results.

AB - Two dimensional Raman scattering images of the density field in a supersonic dry air flow around a sharp-edged wedge are presented. The images are used to characterize the flow field in terms of density, Mach number and angle of attack. Density ratios are determined both from geometrical features (shock angles) as well as directly from the Raman intensity distribution, yielding consistent results.

U2 - 10.2514/6.2001-702

DO - 10.2514/6.2001-702

M3 - Paper

AN - SCOPUS:84897867868

T2 - 39th Aerospace Sciences Meeting and Exhibit 2001

Y2 - 8 January 2001 through 11 January 2001

ER -

Flow field characterization around test objects in a supersonic flow

Abstract

Conference

Access to Document

Handle.net

Fingerprint

Cite this