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12 results

Conference Proceedings

1. Deformation Behavior and Internal Stress of Icosahedral Al-Pd-Mn With Decagonal Phase Lamellae at Elevated Temperatures

Hirai, H. ; Tomita, T. ; Yoshida, F. ; Nakashima, H.

Pub. info.:	Quasicrystals : symposium held November 30-December 2, 1998, Boston, Massachusetts, U.S.A.. pp.331-, 1999. Warrendale, Pa.. MRS - Materials Research Society
Title of ser.:	Materials Research Society symposium proceedings
Ser. no.:	553

Technical Paper

2. AN EXPERIMENTAL STUDY ON A 14 kN LINEAR AEROSPIKE-NOZZLE COMBUSTOR

Sakamoto, H. ; Takahashi, M. ; Sasaki, M. ; Tomita, T. ; Kusaka, K. ; Tamura, H.

Pub. info.:	AIAA paper. pp.1-8, 1999. American Institute of Aeronautics and Astronautics
Title of ser.:	AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Ser. no.:	1999

Technical Paper

3. Effects of base bleed on thrust performance of a linear aerospike nozzle

Tomita, T. ; Takahashi, M. ; Onodera, T. ; Tamura, H.

Pub. info.:	AIAA paper. pp.1-9, 1999. American Institute of Aeronautics and Astronautics
Title of ser.:	AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Ser. no.:	1999

Technical Paper

4. Experimental study on combustion stability characteristics of non-swirl coaxial injectors

Sasaki, M. ; Sakamoto, H. ; Takahashi, M. ; Tomita, T. ; Tamura, H.

Pub. info.:	AIAA paper. pp.1-8, 1998. American Institute of Aeronautics and Astronautics
Title of ser.:	AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Ser. no.:	1998

Technical Paper

5. Visualization of shock wave interaction on the surface of aerospike nozzles

Tomita, T. ; Takahashi, M. ; Onodera, T. ; Tamura, T.

Pub. info.:	AIAA paper. pp.1-10, 1998. American Institute of Aeronautics and Astronautics
Title of ser.:	AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Ser. no.:	1998

Technical Paper

6. Numerical Investigation of the Flow Field Around Linear Aerospike Nozzles

Onodera, T. ; Tomita, T. ; Tamura, H.

Pub. info.:	AIAA paper. pp.1-9, 1999. American Institute of Aeronautics and Astronautics
Title of ser.:	AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Ser. no.:	1999

Technical Paper

7. An experimental study on a 14 kN linear aerospike-nozzle combustor

Sakamoto, H. ; Takahashi, M. ; Sasaki, M. ; Tomita, T. ; Kusaka, K. ; Tamura, H.

Pub. info.:	AIAA paper. pp.1-8, 1999. American Institute of Aeronautics and Astronautics
Title of ser.:	AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Ser. no.:	1999

Technical Paper

8. Comparative study of recessed and non-recessed swirl coaxial injectors

Sasaki, M. ; Sakamoto, H. ; Takahashi, M. ; Tomita, T. ; Tamura, H.

Pub. info.:	AIAA paper. pp.1-7, 1997. American Institute of Aeronautics and Astronautics
Title of ser.:	AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Ser. no.:	1997

Technical Paper

9. LOX/LH2 subscale swirl coaxial injector testing

Tamura, H. ; Sakamoto, H. ; Takahashi, M. ; Sasaki, M. ; Tomita, T. ; Nagao, R.

Pub. info.:	AIAA paper. pp.1-6, 1997. American Institute of Aeronautics and Astronautics
Title of ser.:	AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Ser. no.:	1997

10.

Technical Paper

10. Numerical investigation of the flow field around linear aerospike nozzles

Onodera, T. ; Tomita, T. ; Tamura, H.

Pub. info.:	AIAA paper. pp.1-9, 1999. American Institute of Aeronautics and Astronautics
Title of ser.:	AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Ser. no.:	1999

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