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1

[American Institute of Aeronautics and Astronautics 7th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization - St. Louis,MO,U.S.A. (02 September 1998 - 04 September 1998)] 7th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization - Coupled aero-structural model - Approach and application to high aspect-ratio wing-box structures

Onishi, Ryoichi, Kimura, Toshiya, Guo, Zhihong, Iwamiya, Toshiyuki

Year:

1998

Language:

english

File:

PDF, 783 KB

english, 1998

2

Flow simulation of NAL experimental supersonic airplane/booster separation using overset unstructured grids

Fumiya Togashi, Kazuhiro Nakahashi, Yasushi Ito, Toshiyuki Iwamiya, Yuichi Shimbo

Journal:

Computers & Fluids

Year:

2001

Language:

english

File:

PDF, 984 KB

english, 2001

3

[American Institute of Aeronautics and Astronautics 17th Applied Aerodynamics Conference - Norfolk,VA,U.S.A. (28 June 1999 - 01 July 1999)] 17th Applied Aerodynamics Conference - Analytical model for aero-structural interaction problem of a wing-box structure

Onishi, Ryoichi, Kimura, Toshiya, Guo, Zhihong, Iwamiya, Toshiyuki

Year:

1999

Language:

english

File:

PDF, 789 KB

english, 1999

4

[American Institute of Aeronautics and Astronautics 18th Applied Aerodynamics Conference - Denver,CO,U.S.A. (14 August 2000 - 17 August 2000)] 18th Applied Aerodynamics Conference - Computational aero-structural dynamics for wing with skin-spar-rib construction

Onishi, Ryoichi, Kimura, Toshiya, Guo, Zhihong, Iwamiya, Toshiyuki

Year:

2000

Language:

english

File:

PDF, 865 KB

english, 2000

5

[American Institute of Aeronautics and Astronautics 19th AIAA Applied Aerodynamics Conference - Anaheim,CA,U.S.A. (11 June 2001 - 14 June 2001)] 19th AIAA Applied Aerodynamics Conference - Fuselage shape optimization of a wing-body configuration with nacelles

Makino, Yoshikazu, Iwamiya, Toshiyuki, Lei, Zhong

Year:

2001

Language:

english

File:

PDF, 709 KB

english, 2001

6

Fuselage Shape Optimization of a Wing-Body Configuration with Nacelles

Makino, Yoshikazu, Iwamiya, Toshiyuki, Lei, Zhong

Journal:

Journal of Aircraft

Year:

2003

Language:

english

File:

PDF, 505 KB

english, 2003

7

Anglo-Iranian Oil Co. Case (Jurisdiction), United Kingdom v. Iran.

Collaboration, Nal-Yamagata, Aiso, Hideaki, Fukuda, Masahiro, Iwamiya, Toshiyuki, Nakamura, Atsushi, Nakamura, Takashi, Yoshida, Masahiro

Journal:

The American Journal of International Law

Year:

1952

Language:

english

File:

PDF, 1.61 MB

english, 1952

8

Flow Simulation of NAL Experimental Supersonic Airplane/Booster Separation Using Overset Unstructured Grids.

TOGASHI, Fumiya, NAKAHASHI, Kazuhiro, ITO, Yasushi, MORINO, Hiroyuki, IWAMIYA, Toshiyuki

Journal:

JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

Year:

2000

Language:

english

File:

PDF, 3.70 MB

english, 2000

9

Viscous flow computations of aircraft with changing control surface deflection using unstructured dynamic meshes

Mitsuhiro Murayama, Yasushi Ito, Kazuhiro Nakahashi, Kisa Matsushima, Toshiyuki Iwamiya

Journal:

International Journal for Numerical Methods in Fluids

Year:

2006

Language:

english

File:

PDF, 1.08 MB

english, 2006

10

On the class of nonlinear evolution operators in Banach space

Toshiyuki Iwamiya, Shinnosuke Oharu, Tadayasu Takahashi

Journal:

Nonlinear Analysis: Theory, Methods & Applications

Year:

1986

Language:

english

File:

PDF, 1.35 MB

english, 1986

11

Monotonicity, resolvents and Yosida approximations of operators on Hilbert manifolds

Toshiyuki Iwamiya, Hiroko Okochi

Journal:

Nonlinear Analysis: Theory, Methods & Applications

Year:

2003

Language:

english

File:

PDF, 124 KB

english, 2003

12

Wing design for supersonic transports using integral equation method

Kisa Matsushima, Toshiyuki Iwamiya, Kazuhiro Nakahashi

Journal:

Engineering Analysis with Boundary Elements

Year:

2004

Language:

english

File:

PDF, 663 KB

english, 2004

13

[American Institute of Aeronautics and Astronautics 15th Applied Aerodynamics Conference - Atlanta,GA,U.S.A. (23 June 1997 - 25 June 1997)] 15th Applied Aerodynamics Conference - The effect of nose bluntness of a low-boom configuration on sonic-boom

Makino, Yoshikazu, Sugiura, Takaaki, Watanuki, Tadaharu, Kubota, Hirotoshi, Aoyama, Takashi, Iwamiya, Toshiyuki, Makino, Yoshikazu, Sugiura, Takaaki, Watanuki, Tadaharu, Kubota, Hirotoshi, Aoyama, Tak

Year:

1997

Language:

english

File:

PDF, 619 KB

english, 1997

14

[American Institute of Aeronautics and Astronautics 4th AIAA/CEAS Aeroacoustics Conference - Toulouse,France (02 June 1998 - 04 June 1998)] 4th AIAA/CEAS Aeroacoustics Conference - Low-boom design method by numerical optimization

Makino, Yoshikazu, Watanuki, Tadaharu, Kubota, Hirotoshi, Aoyama, Takashi, Iwamiya, Toshiyuki

Year:

1998

Language:

english

File:

PDF, 605 KB

english, 1998

15

[American Institute of Aeronautics and Astronautics 36th AIAA Aerospace Sciences Meeting and Exhibit - Reno,NV,U.S.A. (12 January 1998 - 15 January 1998)] 36th AIAA Aerospace Sciences Meeting and Exhibit - Inverse design method for wings of supersonic transport

Jeong, Shinkyu, Matsushima, Kisa, Iwamiya, Toshiyuki, Obayashi, Shigeru, Nakahashi, Kazuhiro

Year:

1998

Language:

english

File:

PDF, 586 KB

english, 1998

16

[American Institute of Aeronautics and Astronautics 38th Aerospace Sciences Meeting and Exhibit - Reno,NV,U.S.A. (10 January 2000 - 13 January 2000)] 38th Aerospace Sciences Meeting and Exhibit - Flow simulation of NAL experimental supersonic airplane/booster separation using overset unstructured grids

Togashi, Fumiya, Nakahashi, Kazuhiro, Ito, Yasushi, Iwamiya, Toshiyuki, Shimbo, Yuichi

Year:

2000

Language:

english

File:

PDF, 2.19 MB

english, 2000

17

[American Institute of Aeronautics and Astronautics 38th Aerospace Sciences Meeting and Exhibit - Reno,NV,U.S.A. (10 January 2000 - 13 January 2000)] 38th Aerospace Sciences Meeting and Exhibit - Numerical simulation and aerodynamic design of an SST configuration with nacelles

Makino, Yoshikazu, Iwamiya, Toshiyuki

Year:

2000

Language:

english

File:

PDF, 690 KB

english, 2000

18

[American Institute of Aeronautics and Astronautics 39th Aerospace Sciences Meeting and Exhibit - Reno,NV,U.S.A. (08 January 2001 - 11 January 2001)] 39th Aerospace Sciences Meeting and Exhibit - Aerodynamics evaluation of NAL experimental supersonic airplane in ascent using CFD

Fujita, Takeshi, Ito, Yasushi, Nakahashi, Kazuhiro, Iwamiya, Toshiyuki

Year:

2001

Language:

english

File:

PDF, 1.08 MB

english, 2001

19

[American Institute of Aeronautics and Astronautics 32nd AIAA Fluid Dynamics Conference and Exhibit - St. Louis, Missouri (24 June 2002 - 26 June 2002)] 32nd AIAA Fluid Dynamics Conference and Exhibit - A Computational Study on Unmanned Scaled Supersonic Experimental Airplane

Iwamiya, Toshiyuki

Year:

2002

Language:

english

File:

PDF, 307 KB

english, 2002

20

[American Institute of Aeronautics and Astronautics 21st AIAA Applied Aerodynamics Conference - Orlando, Florida ()] 21st AIAA Applied Aerodynamics Conference - Analysis of Flows over a SST Wing-Body Configuration at Low Speed and High Angles of Attack

Lei, Zhong, Kwak, Dong-youn, Noguchi, Masayoshi, Iwamiya, Toshiyuki

Year:

2003

Language:

english

File:

PDF, 656 KB

english, 2003

21

[American Institute of Aeronautics and Astronautics 21st AIAA Applied Aerodynamics Conference - Orlando, Florida ()] 21st AIAA Applied Aerodynamics Conference - Viscous Flow Computations of Aircraft with Changing Control Surface Deflection Using Unstructured Grids

Murayama, Mitsuhiro, Ito, Yasushi, Nakahashi, Kazuhiro, Matsushima, Kisa, Iwamiya, Toshiyuki

Year:

2003

Language:

english

File:

PDF, 2.96 MB

english, 2003

22

[American Institute of Aeronautics and Astronautics 16th AIAA Applied Aerodynamics Conference - Albuquerque,NM,U.S.A. (15 June 1998 - 18 June 1998)] 16th AIAA Applied Aerodynamics Conference - Computational aeroelastics by coupling compressible fluid equations with shell finite-element structure

Onishi, Ryoichi, Kimura, Toshiya, Guo, Zhihong, Iwamiya, Toshiyuki

Year:

1998

Language:

english

File:

PDF, 669 KB

english, 1998

23

Computational Fluid Dynamics Evaluation of National Aerospace Laboratory Experimental Supersonic Airplane in Ascent

Fujita, Takeshi, Ito, Yasushi, Nakahashi, Kazuhiro, Iwamiya, Toshiyuki

Journal:

Journal of Aircraft

Year:

2002

Language:

english

File:

PDF, 1.03 MB

english, 2002

24

Inverse Design Method for Transonic Multiple Wing Systems Using Integral Equations

Matsushima, Kisa, Takanashi, Susumu, Iwamiya, Toshiyuki

Journal:

Journal of Aircraft

Year:

1997

Language:

english

File:

PDF, 300 KB

english, 1997

25

Numerical Optimization of Fuselage Geometry to Modify Sonic-Boom Signature

Makino, Yoshikazu, Aoyama, Takashi, Iwamiya, Toshiyuki, Watanuki, Tadaharu, Kubota, Hirotoshi

Journal:

Journal of Aircraft

Year:

1999

Language:

english

File:

PDF, 386 KB

english, 1999

26

Gauge Fixing and Gluon Propagators

Collaboration, Nal-Yamagata, Aiso, Hideaki, Fukuda, Masahiro, Iwamiya, Toshiyuki, Nakamura, Atsushi, Nakamura, Takashi, Yoshida, Masahiro

Journal:

Progress of Theoretical Physics Supplement

Year:

1996

Language:

english

File:

PDF, 518 KB

english, 1996

27

Numerical Wind Tunnel (NWT) Project

Iwamiya, Toshiyuki, Nakamura, Takashi, Yoshida, Masahiro

Journal:

Progress of Theoretical Physics Supplement

Year:

1996

Language:

english

File:

PDF, 2.80 MB

english, 1996

28

Inverse Design of Supersonic Airfoils Using Integral Equations

Jeong, Shinkyu, Matsushima, Kisa, Iwamiya, Toshiyuki, Obayashi, Shigeru, Nakahashi, Kazuhiro

Journal:

Journal of Aircraft

Year:

1999

Language:

english

File:

PDF, 126 KB

english, 1999

29

[ACM Press the 1996 ACM/IEEE conference - Pittsburgh, Pennsylvania, United States (1996..-..)] Proceedings of the 1996 ACM/IEEE conference on Supercomputing (CDROM) - Supercomputing '96 - Simulation of the 3 dimensional cascade flow with numerical wind tunnel (NWT)

Nakamura, Takashi, Iwamiya, Toshiyuki, Yoshida, Masahiro, Matsuo, Yuichi, Fukuda, Masahiro

Year:

1996

Language:

english

File:

PDF, 118 KB

english, 1996

30

Flow Simulation of NAL Experimental Supersonic Airplane/Booster Separation Using Overset Unstructured Grids.

TOGASHI, Fumiya, NAKAHASHI, Kazuhiro, ITO, Yasushi, MORINO, Hiroyuki, IWAMIYA, Toshiyuki

Journal:

JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

Year:

2000

File:

PDF, 3.70 MB

2000