1887
banner image
No data available.
Please log in to see this content.
You have no subscription access to this content.
No metrics data to plot.
The attempt to load metrics for this article has failed.
The attempt to plot a graph for these metrics has failed.
Experimental investigations on the magneto-hydro-dynamic interaction around a blunt body in a hypersonic unseeded air flow
Rent:
Rent this article for
USD
10.1063/1.4764105
/content/aip/journal/jap/112/9/10.1063/1.4764105
http://aip.metastore.ingenta.com/content/aip/journal/jap/112/9/10.1063/1.4764105

Figures

Image of FIG. 1.
FIG. 1.

Nozzle flow: Mach number distribution.

Image of FIG. 2.
FIG. 2.

Nozzle flow: temperature distribution.

Image of FIG. 3.
FIG. 3.

Grid (a), temperature and Mach number distributions in front of the test article (b).

Image of FIG. 4.
FIG. 4.

Ionization degree a along the stagnation line.

Image of FIG. 5.
FIG. 5.

Test article and pressure tap positions.

Image of FIG. 6.
FIG. 6.

Magnet coil.

Image of FIG. 7.
FIG. 7.

Test article design.

Image of FIG. 8.
FIG. 8.

Magnetic flux density field B around the magnet.

Image of FIG. 9.
FIG. 9.

Computed and measured normal component of magnetic flux density field Bn.

Image of FIG. 10.
FIG. 10.

Cooling system view.

Image of FIG. 11.
FIG. 11.

Test article exploded view.

Image of FIG. 12.
FIG. 12.

SCIROCCO plasma wind tunnel aerial view.

Image of FIG. 13.
FIG. 13.

SCIROCCO functional scheme.

Image of FIG. 14.
FIG. 14.

SCIROCCO performance map.

Image of FIG. 15.
FIG. 15.

Test article during the experiment (magnet off).

Image of FIG. 16.
FIG. 16.

Test article during the experiment (magnet on).

Image of FIG. 17.
FIG. 17.

Stagnation pressure versus time.

Image of FIG. 18.
FIG. 18.

Normalized pressure during test no. 1.

Image of FIG. 19.
FIG. 19.

Pressure tap 5: normalized pressure during test no.1.

Image of FIG. 20.
FIG. 20.

Pressure tap 5: percentage variation of the normalized pressure during test No.1.

Image of FIG. 21.
FIG. 21.

Pressure tap 5: normalized pressure during test no. 2.

Image of FIG. 22.
FIG. 22.

Pressure tap 5: normalized pressure during test no. 2.

Image of FIG. 23.
FIG. 23.

Spot location for the temperature history in test no. 2.

Image of FIG. 24.
FIG. 24.

Spot temperature versus time in test no. 2.

Image of FIG. 25.
FIG. 25.

Cooling water temperature during test no. 1: inlet temperature (dashed) and temperature outlet (continuous).

Tables

Generic image for table
Table I.

Computed mass fractions in the reservoir.

Generic image for table
Table II.

Nominal test conditions.

Loading

Article metrics loading...

/content/aip/journal/jap/112/9/10.1063/1.4764105
2012-11-02
2014-04-24
Loading

Full text loading...

This is a required field
Please enter a valid email address
752b84549af89a08dbdd7fdb8b9568b5 journal.articlezxybnytfddd
Scitation: Experimental investigations on the magneto-hydro-dynamic interaction around a blunt body in a hypersonic unseeded air flow
http://aip.metastore.ingenta.com/content/aip/journal/jap/112/9/10.1063/1.4764105
10.1063/1.4764105
SEARCH_EXPAND_ITEM