There is a technical and economical need for a correction method to scale model test data, which fulfills five tasks: It should be (i) physically based, (ii) understandable and easy to apply, and (iii) universal, i.e., applicable to centrifugal as well as to axial machines of different specific speed. Moreover, the method should (iv) account for the aerodynamic quality of the machine and should (v) be reliable not only at peak efficiency, but also at off-design condition. Up to now, no method meets all five tasks. To fill that gap, a method developed at Technical University Darmstadt together with Forschungsvereinigung für Luft- und Trocknungstechnik e. V. (FLT) is introduced in this work. The method consists of three steps: Assuming the so-called master curve, scaling the efficiency itself and shifting the best efficiency point to a higher flow coefficient. For each step, a simple physical explanation is given. The validation of the method is done with test data of two axial fans with four different stagger angles and two centrifugal fans. In spite of its simplicity, the method shows a good agreement to test data compared with traditional and most recent scaling methods. A short overview about the advantages and disadvantages of compared methods and a conclusion is given at the end of this work.

References

1.
Falkner
,
H.
,
2008
, “
Water Pumps (in Commercial Buildings, Drinking Water Pumping, Food Industry, Agriculture)
,” Report to European Commission, Appendix 5, Lot 11.
2.
European Association of Pump Manufacturers
,
1999
,
Attainable Efficiencies of Volute Casing Pumps: A Reference Guide
,
Elsevier Science
,
Kidlington
, UK.
3.
Pfleiderer
,
C.
,
1955
,
Die Kreiselpumpen für Flüssigkeiten und Gase
,
Springer
,
Berlin
.
4.
Mühlemann
,
E.
,
1948
, “
Zur Aufwertung des Wirkungsgrads von Überdruck-Wasserturbinen
,”
Schweiz. Bauzeitung
,
66
, pp.
331
333
.
5.
Hess
,
M.
, and
Pelz
,
P.
,
2010
, “
On Reliable Performance Prediction of Axial Turbomachines
,” ASME Turbo Expo 2010: Power for Land, Sea, and Air (GT2010) Glasgow, UK, June 14–18,
ASME
Paper No. GT2010-22290.10.1115/GT2010-22290
6.
Casey
,
M.
, and
Robinson
,
C.
,
2011
, “
A Unified Correction Method for Reynolds Number, Size and Roughness Effects on the Performance of Compressors
,”
Proc. Inst. Mech. Eng., Part A
,
225
(
7
), pp.
864
876
.10.1177/0957650911410161
7.
Hess
,
M.
,
2010
, “
Aufwertung bei Axialventilatoren—Einfluss von Reynolds-Zahl, Rauheit, Spalt und Betriebspunkt auf Wirkungsgrad und Druckziffer
,” Ph.D. thesis, Technische Universität Darmstadt, Darmstadt, Germany.
8.
Spurk
,
J.
,
1992
,
Dimensionsanalyse in der Strömungslehre
,
Springer
,
Berlin
.
9.
Colebrook
,
C.
,
1937
, “
Experiments With Fluid Friction in Roughened Pipes
,”
Proc. R. Soc. London
,
161
(
906
), pp.
367
381
.10.1098/rspa.1937.0150
10.
Schlichting
,
H.
, and
Scholz
,
N.
,
1950
, “
Über die theoretische Berechnung der Strömungsverluste eines ebenen Schaufelgitters
,”
Ing.-Arch.
,
19
, pp.
42
65
.10.1007/BF00534669
11.
Stonjek
,
S.
,
2010
, Vorbereitende Arbeiten zur Wirkungsgradaufwertung an Radialventilatoren, Abschlussbericht L232, Forschungsgemeinschaft für Luft- und Trocknungstechnik, Frankfurt a. M, technical report.
12.
Deutsches Institut für Normung (DIN)
,
1985
, Ventilatoren—Leistungsmessung, Normkennlinien, DIN 24163 Teil 1-3, Deutsches Institut für Normung (DIN).
13.
Verein Deutscher Ingenieure (VDI)
,
2002
, Abnahme- und Leistungsversuche an Ventilatoren (VDI-Ventilatorregeln), VDI 2044, Verein Deutscher Ingenieure (VDI).
14.
Karstadt
,
S.
, and
Pelz
,
P.
,
2012
, “
A Physical Model for the Tip Vortex Loss—Experimental Validation and Scaling Method
,” Proc. of ASME Turbo Expo 2012, Copenhagen, Denmark, June 11-15, ASME Paper No. GT2012-68397.
15.
Nakhjiri
,
M.
,
Pelz
,
P.
,
Matyschok
,
B.
,
Däubler
,
L.
, and
Horn
,
A.
,
2012
, “
Apparent and Real Efficiency of Turbochargers Under Influence of Heat Flow
,” 14th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC-14), Honolulu, HI, February 27–March 2.
You do not currently have access to this content.