Blank Cover Image

Numerical Investigation of a Low Reynolds Number Flow Field in a Turbine Blade Row

Author(s):
Publication title:
AIAA paper
Title of ser.:
AIAA Paper : Aerospace Sciences Meeting and Exhibit
Ser. no.:
2001
Pub. Year:
2001
No.:
2001-0524
Paper no.:
AIAA-2001-0524
Page(from):
1
Page(to):
7
Pages:
7
Pub. info.:
American Institute of Aeronautics and Astronautics
ISSN:
01463705
Language:
English
Call no.:
A07400
Type:
Technical Paper

Similar Items:

1 Technical Paper Numerical and experimental investigation of low Reynolds number effects on laminar flow separation and transition an a cascade of compressor blades

Enomoto, Shunji, Hah, C., Hobson, G. V.

American Society of Mechanical Engineers
7 Technical Paper Experimental and Numerical Investigation of Losses in Low-Pressure Turbine Blade Rows

Dorney, Daniel J., Lake, James P., King, Paul I., Ashpis, David E.

American Institute of Aeronautics and Astronautics
2 Technical Paper Development of hub corner stall and its influence on the performance of axial compressor blade rows

Hah, Chunill, Loellbach, James

The American Society of Mechanical Engineers
8 Technical Paper A Three-Dimensional Structured/Unstructured Hyblid Navier-Stokes Method for Turbine Blade Rows

Tsung, F.-L., Loellbach, J., Kwon, O., Hah, C.

National Aeronautics and Space Adminstration
3 Technical Paper Numerical study of the tip clearance flow development in a propulsion pump stage

Lee, Yu-Tai, Hah, Chunill, Loellbach, James

The American Society of Mechanical Engineers
9 Conference Proceedings A Numerical Investigation of the Interaction Between Rotor Bow Waves and Upstream Wake Generators in a Transonic Compressor Stage

Gregory Bloch, James Loellbach, Chunill Hah

American Society of Mechanical Engineers
4 Technical Paper Flow analyses in a single-stage propulsion pump

Lee, Yu-Tai, Hah, Chunill, Loellbach, James

The American Society of Mechanical Engineers
10 Technical Paper An Experimental investigation of heat transfer, transition and separation on turbine blades at low reynolds number and high turbulence intensity

Baughn, James W., Butler, Robert J., Byerley, Aaron R., Rivir, Richard B.

The American Society of Mechanical Engineers
5 Technical Paper Unsteady flow interaction inside a High-Reynolds-Number, axial-flow pump stage

Lee, Y., Hah, C., Loellbach, J.

American Institute of Aeronautics and Astronautics
11 Technical Paper Analysis of transonic flow fields inside a high pressure ratio centrifugal compressor at design and off design conditions

Hah, Chunill, Krain, Hartmut

The American Society of Mechanical Engineers
6 Technical Paper Unsteady Flow Analysis Of RLV Pump Stage at Design and Off-Design Conditions

Hah,Chunill, Loellbach,James, Owen,Albert, Khandelwal,Suresh

American Institute of Aeronautics and Astronautics
12 Technical Paper Study of low Reynolds number effects on the losses in low-pressure turbine blade rows

Dorney, D.J., Ashpis, D.E.

American Institute of Aeronautics and Astronautics
1
 
2
 
3
 
4
 
5
 
6
 
7
 
8
 
9
 
10
 
11
 
12