Comparative study of recessed and non-recessed swirl coaxial injectors

Comparative study of recessed and non-recessed swirl coaxial injectors

Author(s):

Sasaki, M. ( National Aerospace Laboratory, KRC, Japan )
Sakamoto, H.
Takahashi, M.
Tomita, T.
Tamura, H.

Publication title:

AIAA paper

Title of ser.:

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

Ser. no.:

1997

Pub. Year:

1997

No.:

97-2907

Paper no.:

97-2907

Page(from):

1

Page(to):

7

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050849
Series ID:	PA00000151
Conf. info. (Name):	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Conf. info. (Number):	33rd
Conf. info. (Venue):	Seattle, WA
Conf. info. (Date):	1997.07.06-1997.07.09
Note for article:	33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, July 6-9, 1997/Seattle, WA

Similar Items:

1 Technical Paper Experimental study on combustion stability characteristics of non-swirl coaxial injectors Sasaki, M., Sakamoto, H., Takahashi, M., Tomita, T., Tamura, H. American Institute of Aeronautics and Astronautics	7 Technical Paper An Experimental Study of Super-Pulsating Flow on a Shear Coaxial Injector with a Recessed Inner Post Y. Nunome, H. Sakamoto, H. Tamura, A. Kumakawa, S. Amagasaki, T. Inamura American Institute of Aeronautics and Astronautics
2 Technical Paper LOX/LH2 subscale swirl coaxial injector testing Tamura, H., Sakamoto, H., Takahashi, M., Sasaki, M., Tomita, T., Nagao, R. American Institute of Aeronautics and Astronautics	8 Technical Paper Parametric Study on the Influence of a Discontinuous Step in a Nozzle Contour on Side-Load Tomita, T., Takahashi, M., Sasaki, M., Tamura, H., Watanabe, Y. American Institute of Aeronautics and Astronautics
3 Technical Paper Sub-Scale Nozzle Combustion Tests of the LE-7A Engine for Clarification of Large Side-Load (I) Formation of RSS Structure Due to Combustion Condition. Tomita, T., Sakamoto, H., Takahashi, M., Sasaki, M., Tamura, H. American Institute of Aeronautics and Astronautics	9 Technical Paper Experimental and Numerical Study on Characteristics of Fuel Mixers for a Liquid Rocket Engine T. Onodera, T. Tomita, M. Takahashi, M. Sasaki, H. Sakamoto, T. Kimura American Institute of Aeronautics and Astronautics
4 Technical Paper Sub-scale Nozzle Combustion Tests of the LE-7A Engine for Clarification of Large Side-Load (II) Influence of a Step in Nozzle Contour on Side-Ioad. Tomita, T., Sakamoto, H., Takahashi, M., Sasaki, M., Tamura, H. American Institute of Aeronautics and Astronautics	10 Technical Paper Influence of a Gap for Film Cooling on Transient Flow Characteristics of Rocket Engine Nozzles. Takahashi, M., Tomita, T., Sakamoto, H., Tamura, H., Watanabe, Y. American Institute of Aeronautics and Astronautics
5 Technical Paper AN EXPERIMENTAL STUDY ON A 14 kN LINEAR AEROSPIKE-NOZZLE COMBUSTOR Sakamoto, H., Takahashi, M., Sasaki, M., Tomita, T., Kusaka, K., Tamura, H. American Institute of Aeronautics and Astronautics	11 Technical Paper Strong Side-Load Observed on a Parabolic Nozzle with No RSS Flow Pattern Tomita, T., Takahashi, M., Sasaki, M., Tamura, H. American Institute of Aeronautics and Astronautics
6 Technical Paper An experimental study on a 14 kN linear aerospike-nozzle combustor Sakamoto, H., Takahashi, M., Sasaki, M., Tomita, T., Kusaka, K., Tamura, H. American Institute of Aeronautics and Astronautics	12 Technical Paper Investigation on Characteristics of Conventional-Nozzle-Based Altitude Compensating Nozzles by Cold-Flow Tests T. Tomita, M. Takahashi, M. Sasaki, H. Tamura American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12