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46 results

Technical Paper

1. Flight effects on high speed jet noise in a two-dimensional mixer-ejector nozzle

Dravet, A. ; Julliard, J. ; Nakamura, Y. ; Oishi, T.

Pub. info.:	AIAA paper. pp.1-7, 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

2. Reflected Shock Wave/Boundary Layer Interaction in High-Enthalpy Shock Tunnel

Kaneko, M. ; Men'shov, I. ; Nakamura, Y.

Pub. info.:	AIAA paper. pp.1-9, 2000. American Institute of Aeronautics and Astronautics
Title of ser.:	AIAA Paper : Fluids Conference and Exhibit
Ser. no.:	2000

Technical Paper

3. Anisotropic Cartesian Grid Adaptation

Lahur, P.R. ; Nakamura, Y.

Pub. info.:	AIAA paper. pp.1-11, 2000. American Institute of Aeronautics and Astronautics
Title of ser.:	AIAA Paper : Fluids Conference and Exhibit
Ser. no.:	2000

Technical Paper

4. Number density measurement of excited argon gas around a blunt body

Kawazoe, H. ; Nakamura, Y. ; Hamamoto, N. ; Ohara, M.

Pub. info.:	AIAA paper. pp.1-11, 1996. American Institute of Aeronautics and Astronautics
Title of ser.:	AIAA Paper : Aerospace Sciences Meeting and Exhibit
Ser. no.:	1996

Technical Paper

5. Three dimensional shock/boundary layer interaction between a rocket and SRB

Tanahashi, Y. ; Ohara, T. ; Nakamura, Y.

Pub. info.:	AIAA paper. pp.1-11, 1997. American Institute of Aeronautics and Astronautics
Title of ser.:	AIAA Paper : AIAA Thermophysics Conference
Ser. no.:	1997

Technical Paper

6. Heat transfer calculation of blunt bodies in nonequilibrium air flows

Hamamoto, N. ; Lee, M.G. ; Nakamura, Y. ; Men'shov, I.

Pub. info.:	AIAA paper. pp.1-11, 1997. American Institute of Aeronautics and Astronautics
Title of ser.:	AIAA Paper : AIAA Fluid Dynamics Conference
Ser. no.:	1997

Technical Paper

7. The new method of crankshaft design for high-speed diesel engines

Nakamura, Y. ; Ito, M. ; Morita, K. ; Numata, A. ; Shimokouchi, H. ; Arakawa, H.

Pub. info.:	A.S.M.E. paper. 1993. New York, NY. The American Society of Mechanical Engineers
Title of ser.:	ASME Technical Paper : ICE
Ser. no.:	1993

Technical Paper

8. Computation of Nozzle Starting Process with Thermal and Chemical Nonequilibrium in High-Enthalpy Shock Tunnel.

Kaneko, M. ; Nakamura, Y. ; Men'shov, I.

Pub. info.:	AIAA paper. 2002. American Institute of Aeronautics and Astronautics
Title of ser.:	AIAA Paper : Aerospace Sciences Meeting and Exhibit
Ser. no.:	2002

Technical Paper

9. The Effects of Attack Angle on Side Jet Aerodynamic Interaction in a Blunted Body at Hypersonic Flow.

Kurita, M. ; Okada, T. ; Nakamura, Y.

Pub. info.:	AIAA paper. 2001. Reston, VA. American Institute of Aeronautics and Astronautics
Title of ser.:	AIAA Paper : International Space Planes and Hypersonic Systems and Technologies Conference
Ser. no.:	2001

10.

Technical Paper

10. A Device for Reduction of Heat Flux Produced by Hypersonic Shock Interference

Kitamura, K. ; Nishino, A. ; Ishikawa, T. ; Men'shov, I. ; Nakamura, Y.

Pub. info.:	AIAA meeting papers on disc. 2004. [Reston, Va.]. American Institute of Aeronautics and Astronautics
Title of ser.:	AIAA Paper : AIAA Fluid Dynamics Conference
Ser. no.:	34th

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