Fuel-vortex interactions for enhanced mixing in supersonic flow

Fuel-vortex interactions for enhanced mixing in supersonic flow

Author(s):

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Ser. no.:

1996

Pub. Year:

1996

No.:

96-2661

Paper no.:

96-2661

Page(from):

1

Page(to):

14

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050840
Series ID:	PA00000151
Conf. info. (Name):	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Conf. info. (Number):	32nd
Conf. info. (Venue):	Lake Buena Vista, FL
Conf. info. (Date):	1996.07.01-1996.07.03
Note for article:	32nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, July 1-3, 1996/Lake Buena Vista, FL

Similar Items:

1 Technical Paper Interaction of jets and shear layers to produce instabilities and mixing enhancement in supersonic flows King, P.S., Schetz, J.A. American Institute of Aeronautics and Astronautics	7 Technical Paper Effects of injection angle on the breakup processes of liquid jets in subsonic crossflows Fuller, R., Wu, P.-K., Kirkendall, K., Nejad, A. American Institute of Aeronautics and Astronautics
2 Technical Paper Jet Interaction in Supersonic Flow with a Surface Ramp Byun, Y., Wallis, S., Viti, V., Bae, K., Schetz, J., Bowersox, R. American Institute of Aeronautics and Astronautics	8 Technical Paper Expansion and mixing processes of underexpanded supercritical fuel jets injected into superheated conditions Wu, P.-K., Shahnam, M., Kirkendall, K., Carter, C., Nejad, A. American Institute of Aeronautics and Astronautics
3 Technical Paper An investigation of advanced fuel injection schemes for scramjet combustion Baurle, R.A., Fuller, R.P., White, J.A., Chen, T.H., Gruber, M.R., Nejad, A.S. American Institute of Aeronautics and Astronautics	9 Technical Paper Integrated CFD and experimental studies of complex injectors in supersonic flows (Invited) Schetz, Joseph A., Fuller, Raymond American Institute of Aeronautics and Astronautics
4 Technical Paper Development of a pressure-fed rocket engine using hydrogen peroxide and JP-8 Wu, P.-K., Fuller, R.P., Morlan, P.W., Ruttle, D.W., Nejad, A.S., Anderson, W.E. American Institute of Aeronautics and Astronautics	10 Technical Paper Investigation of Supersonic Mixing Control Using Cavities: effect of fuel injection location Burnes, R., Parr, T.P., Wilson, K.J., Yu, K. American Institute of Aeronautics and Astronautics
5 Technical Paper Vortex Interactions with a Jet in a Supersonic Crossflow L. Maddalena, J. Schetz, R. Neel American Institute of Aeronautics and Astronautics	11 Technical Paper An Integrated Aeroramp-Injector/Plasma-Igniter for Hydrocarbon Fuels in Supersonic Flow - Part B: Experimental Studies of the Operating Conditions Gallimore,S., Jacobsen,L., O'Brien,W., Schetz,J. American Institute of Aeronautics and Astronautics
6 Technical Paper Development of a Pressure-Fed Rocket Engine Using Hydrogen Peroxide and JP-8 Wu, P.-K., Fuller, R. P., Morlan, P. W., Ruttle, D. W., Nejad, A. S., Anderson, W. E. American Institute of Aeronautics and Astronautics	12 Technical Paper Studies of Shock Wave/Transverse Injection Interaction on Supersonic Mixing Processes T. Campioli, L. Maddalena, J. Schetz American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12