Analysis and Design of Rectangular-Cross-Section Nozzles for Scramjet Engine Testing

Analysis and Design of Rectangular-Cross-Section Nozzles for Scramjet Engine Testing

著者名:

Gaffney, R. ( NASA Langley Research Center, Hampton, VA )
Korte, J.

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:

2004-1137

ペーパー番号:

AIAA Paper 2004-1137

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 a Mach 3 Nozzle for TBCC Testing in the NASA LaRC 8-Ft High Temperature Tunnel R. Gaffney, A. Norris American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Design, Manufacturing and Test of a Plug Nozzle Rocket Engine. Besnard, E., Chen, H.H., Mueller, T., Garvey, J. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Design of a Mach-15 Total-Enthalpy Nozzle With Non-Uniform Inflow Using Rotatioanl MOC Gaffney, R. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー The Design of a High-Q, Mach-5 Nozzle for the NASA Langley 8-Foot HTT R. Gaffney, B. Stewart, S. Harvin American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Design, fabrication, and calibration of a mach 6.5 hypersonic shock tunnel nozzle for scramjet testing applications Modroukas, D., Betti, A., Chinitz, W., Bakos, R.J. American Institute of Aeronautics and Astronautics	9 テクニカルペーパー CFD studies in support of NWTC test section design Bussoletti, J.E., Huffington, J.R., Krynytzky, A.J., Saaris, G.R. American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Inviscid Design of Hypersonic Wind Tunnel Nozzles for a Real Gas Korte, J. J. American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Development and Testing of the Upgraded High Pressure Turbine Section for an Industrial Gas Turbine. Aschenbruck, E., Frank, D., Korte, T., Muller, R., Orth, U. American Society of Mechanical Engineers
5 テクニカルペーパー Autopilot Design for a Square Cross-section Missile Hyde, R., Cleminson, J. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー HYPERVELOCITY SCRAMJET COMBUSTOR-NOZZLE ANALYSIS AND DESIGN Thompson, H.Doyle, Hoffman, Joe D. National Aeronautics and Space Adminstration
6 テクニカルペーパー Parametric Study of Jets Emanating from Serpentine Nozzles of Varied Cross-Section T. Reynolds, M. Reeder, E. Stephen, R. Maple, J. Crafton American Institute of Aeronautics and Astronautics	12 テクニカルペーパー Investigation of Low-Reynolds-Number Rocket Nozzle Design Using PNS-Based Optimization Procedure Hussaini, M. Moin, Korte, John J. National Aeronautics and Space Adminstration

1

2

3

4

5

6

7

8

9

10

11

12