|
|
|
 |
 |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
In the map collection there are compressor and turbine maps ready for use with GasTurb. The data are stored as ASCII files in such a way that they can be easily converted to any format and then used with other performance computer programs. A broshure contains figures and references for all maps. |
|
|
|
Axial Compressors |
|
|
|
|
Stg No |
Press Ratio |
Flow kg/s |
Reference |
Company Organisation |
|
1 |
1.43 |
66.8 |
Experimental Quiet Engine Program - Summary Report, Fig. 18 (Fan B, core)
W. G. Cornell, NASA CR-2519, 1975 |
NASA/GE |
|
1 |
1.52 |
438 |
Experimental Quiet Engine Program - Summary Report, Fig. 17 (Fan B, bypass)
W. G. Cornell, NASA CR-2519, 1975 |
NASA/GE |
|
1 |
1.6 |
47 |
Simulating Indirect Thrust Measurement Methods for High-Bypass Turbofans
J.D. Stevenson, H.I.H. Saravanamuttoo
Journal of Engineering for Gas Turbines and Power, Jan 1995, Vol. 117, Page 38 |
P&W Canada |
|
1 |
1.6 |
100 |
Extended Parametric Representation of Compressor, Fans and Turbines Vol III,
Pages 15-17: Variable Geometry Settings 0, 20, 40
G.L.Converse
NASA-CR-174647, 1984 |
NASA/GE |
|
1
|
1.6 |
100 |
Extended Parametric Representation of Compressor, Fans and Turbines Vol III
Pages 24-26
G.L.Converse R.G.Giffin
NASA-CR-174645, 1984 |
NASA/GE |
|
1
rotor |
1.7 |
500 |
Method for the Prediction of Supersonic Compressor Blade Performance
C. Freeman
Journal of Propulsion Vol 8 No 1, 1992 |
RR |
|
1 |
2.2 |
40 |
Design and Test of a Low Aspect Ratio Fan Stage
T.L.Creason, S. Baghdadi
AIAA-88-2816, 1988 |
P&W Florida |
|
2 |
3.1 |
2.2 |
Advancement of Small Gas Turbine Component Technology
J.V.Davis E.J.Dellert
USAAVLABS Tech Report 69-10B, 1970 |
Continental |
|
5 |
7 |
15 |
Design and Performance of a Low Aspect Ratio, High Tip Speed, Multi Stage Axial Compressor
W.A.Tesch, R.L.Pase
AIAA 83-1116, 1983 |
P&W Florida |
|
9 |
8.2 |
30 |
Design and Development of an Advanced F100 Compressor
C.M.Love
AGARD CP-421, 1987 |
P&W Florida |
|
8 |
10.2 |
32 |
Advanced Technology's Impact on Compressor Design and Development: A Perspective
C.L. Ball
SAE Paper 892213, 1989 |
NACA |
|
15 |
12 |
27.3 |
Design and Development of a 12:1 Pressure Ratio Compressor for the Ruston 6MW Gas Turbine
F. Carchedi, G.R. Wood
ASME 82-GT-20, 1982 |
Ruston |
|
? |
13 |
25 |
Computer Program for Estimating Performance of Air-Breathing Aircraft Engines (Page 76)
K.A.Geiselhart M.J.Caddy S.J.Morris,Jr.
NASA TM 4254 |
NASA |
|
17 |
14.7 |
36 |
Developments Leading to an Axial Flow Compressor for a 25 MW Class High Efficiency Gas Turbine
Y.Kashiwabara et alii
ASME 90-GT-238, 1990 |
Hitachi |
|
16 |
17 |
63 |
Aerodynamic Development and Performance of the CF6-6 / LM2500 Compressor
J.F. Klapproth, M.L.Miller, D.E. Parker
AIAA 79-7030, 1979 |
GE |
|
10 |
23 |
55 |
Energy Efficient Engine High Pressure Compressor Component Performance Report
S.J. Cline et allii
NASA CR-168245 |
NASA/GE |
|
|
|
|
Radial Compressors |
|
|
|
|
Stg. No |
Press Ratio |
Flow kg/s |
Reference |
Company Organisation |
|
1 |
4.3 |
2.5 |
Extended Parametric Representation of Compressor, Fans and Turbines Vol III
G.L.Converse
NASA-CR-174647, 1984 |
NASA/GE |
|
1 |
6 |
1 |
Experimental Performance of a 16.1 cm Tip Diameter Sweptback Centrifugal Compressor Designed for a 6:1 Pressure Ratio
H.A. Klassen J.R. Wood L.F. Schuman
NASA TMX-3552, 1977 |
NASA |
|
1 |
6 |
0.35 |
The Performance Prediction and Demonstration of a Centrifugal Compressor for the Multi Purpose Small Power Unit
T. Yoshinaka, R.G. Thomson, J. Letourneau
ASME 89-GT-112, 1989 |
P&W Canada |
|
1 |
6 |
2.7 |
Experimental Investigation on Small Turboprop Behavior Under Compressor Rorating Stall for Different Inlet Flow Conditions
S.Colantuoni G.Liotti
AGARD_CP_400 |
Alfa Romeo |
|
1 rotor |
6.1 |
2.6 |
Aerodynamics of a Centrifugal Compressor Impeller with Transsonic Inlet Conditions
H.Krain B.Hoffmann H.Pak
ASME 95-GT-79, 1995 |
DLR Germany |
|
1 |
6 |
0.35 |
The Performance Prediction and Demonstration of a Centrifugal Compressor for the Multiple Purpose Small Power Unit
T.Yoshinaka R.G.Thomson J.Letourneau
ASME 89-GT-112, 1989 |
P&W Canada |
|
1 |
12 |
3 |
Le compresser centrifuge, composant essentiel des turbomoteurs de petite et moyenne puissance (fig.6)
P.Belaygue H.Vigneau
AGARD PEP82, 1993 |
Turbomeca |
|
2 |
14 |
3.5 |
Design and Development of an Advanced Two-Stage Centrifugal Compressor
D.L.Palmer W.F.Waterman
ASME 94-GT-202, 1994 |
Allied Signal |
|
2 |
15 |
3 |
Le compresser centrifuge, composant essentiel des turbomoteurs de petite et moyenne puissance (fig.8)
P.Belaygue H.Vigneau
AGARD PEP82, 1993 |
Turbomeca |
|
|
|
|
Turbines |
|
|
|
|
Stg. No |
Reference |
Company Organisation |
|
2 |
Compressor and Turbine Performance Prediction System Development - Lessons from Thirty Years of History
G.K. Serovy
AGARD LS 83, 1976 |
? |
|
1 |
Extended Parametric Representation of Compressors, Fans and Turbines
Vol. II - User's Manual (Parametric Turbine)
Variable Guide Vane Settings 61°, 68° and 75° (3 Maps)
G.L.Converse
NASA-CR-174646, 1984 |
NASA |
|
1 |
Extended Parametric Representation of Compressors, Fans and Turbines
Vol. II - User's Manual (Parametric Turbine), Page 30-31
Radial Turbine
G.L.Converse
NASA-CR-174646, 1984 |
NASA |
|
|
|
Copyright © 2001 Joachim Kurzke |
|
|
