Performance Characteristics of Scramjet Engine with Different Combustor Shapes at Hypervelocity Condition over Mach 10 Flight

Performance Characteristics of Scramjet Engine with Different Combustor Shapes at Hypervelocity Condition over Mach 10 Flight

Author(s):

M. Takahashi ( JAXA Kakuda Space Center, Kakuda, Miyagi, Japan )

Publication title:

AIAA meeting papers on disc

Title of ser.:

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

Ser. no.:

2007

Pub. Year:

2007

No.:

2007-5395

Paper no.:

AIAA Paper 2007-5395

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200717 [CD-ROM 2007 Disc 17]

Type:

Technical Paper

Details

TDL ID:	ZA00049509
Series ID:	PA00000151
Conf. info. (Name):	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Conf. info. (Number):	43rd
Conf. info. (Venue):	Cincinnati, OH
Conf. info. (Date):	2007.07.08-2007.07.11
Note for article:	43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Cincinnati, OH, July 8-11, 2007

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