The Effects of Swirler Geometry on the Performance of Gas Turbine Combustor Using Planar Imaging Technique

The Effects of Swirler Geometry on the Performance of Gas Turbine Combustor Using Planar Imaging Technique

Author(s):

Koh,H. ( School of Mechanical and Aerospace Engineering Seoul National University )
Kim,D.
Jung,K.
Park,J.-H.
Yoon,Y.

Publication title:

AIAA paper

Title of ser.:

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

Ser. no.:

2001

Pub. Year:

2001

No.:

2001-3757

Paper no.:

AIAA-2001-3757

Page(from):

1

Pub. info.:

Reston, VA: American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050826
Series ID:	PA00000151
Conf. info. (Name):	AIAA/ASME/SAE/ASEE Joint Propulsion Conference (JPC) & Exhibit
Conf. info. (Number):	37th
Conf. info. (Venue):	Salt Lake City, UT
Conf. info. (Date):	2001.07.08-2001.07.11
Note for article:	37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit 8-11 July 2001/Salt Lake City, Utah

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