Aerodynamic Design of 3D Compressor Blade Using an Adjoint Method

Aerodynamic Design of 3D Compressor Blade Using an Adjoint Method

著者名:

Chung, J. ( University of Illinois at Urbana-Champaign, Urbana, IL )
Lee, K.
Martin, G. ( University of Illinois, Urbana, IL )

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

シリーズ巻号:

42nd

発行年:

2004

通号:

2004-0027

ペーパー番号:

AIAA Paper 2004-27

出版情報:

[Reston, Va.]: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200401 [CD-ROM 2004 Disc 1]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00001549
シリーズID:	PA00000138
会議名:	AIAA Aerospace Sciences Meeting and Exhibit
回次:	42nd
会議開催地:	Reno, Nevada
会議開催年:	2004.01.05-2004.01.08

類似資料:

1 テクニカルペーパー Design of 3D Transonic Compressor Blades Using Numerical Optimization Chung, J., Shim, J., Lee, K. D. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー 3D Design of Transonic Axial Compressor Blades with 3D Navier-Stokes Physics Chung,J., Shim,J., Lee,K.D. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Design Optimization of Transonic Compressor Blades Using Quasi-3D Navier-Stokes Physics Chung, J., Lee, K. D. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Shape Optimization of High-Speed Axial Compressor Blades Using 3D Navier-Stokes Flow Physics. Chung, J., Shim, J., Lee, K.D. American Society of Mechanical Engineers
3 テクニカルペーパー Design optimization of transonic compressor blades using quasi-3D Navier-Stokes physics Chung, J., Lee, K.D. American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Helicopter Rotor Design Using a Time-Spectral and Adjoint-Based Method S. Choi, M. Potsdam, K. Lee, G. Iaccarino, J. Alonso American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Inverse Design of 3D Transonic Compressor Blade using 3D Navier-Stokes Flow Physics. Chung, J., Shim, J., Lee, K.D. American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Shape optimization of transonic compressor blades using quasi-3D flow physics Chung, June, Lee, Ki D. American Society of Mechanical Engineers
5 テクニカルペーパー Aerodynamic Performance Enhancement of Turbomachinery Blades Using 3D Flow Physics Chung,J., Shim,J., Lee,K.D. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Compressor Blade Optimization Using a Continuous Adjoint Formulation. Papadimitriou, D.I., Giannakoglou, K.C. American Society of Mechanical Engineers
6 テクニカルペーパー Aerodynamic Design of Cascade Blades Using Asymptotic Solution of Euler Equations. Shim, J., Chung, J., Lee, K.D., Verhoff, A. American Institute of Aeronautics and Astronautics	12 テクニカルペーパー An Efficient Aerodynamic Design Method Using Asymptotic Solutions of the Euler Equations. Shim, J., Lee, K.D., Verhoff, A. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12