An Advanced Balancing Methodology for the Propeller of a Wind-Tunnel Model

VEG, Aleksandar .
An Advanced Balancing Methodology for the Propeller of a Wind-Tunnel Model. 
Strojniški vestnik - Journal of Mechanical Engineering, [S.l.], v. 53, n.5, p. 319-328, november 2017. 
ISSN 0039-2480.
Available at: <https://www.sv-jme.eu/sl/article/an-advanced-balancing-methodology-for-the-propeller-of-a-wind-tunnel-model/>. Date accessed: 23 nov. 2024. 
doi:http://dx.doi.org/.

Veg, A.
(2007).
An Advanced Balancing Methodology for the Propeller of a Wind-Tunnel Model.
Strojniški vestnik - Journal of Mechanical Engineering, 53(5), 319-328.
doi:http://dx.doi.org/

@article{.,
	author = {Aleksandar  Veg},
	title = {An Advanced Balancing Methodology for the Propeller of a Wind-Tunnel Model},
	journal = {Strojniški vestnik - Journal of Mechanical Engineering},
	volume = {53},
	number = {5},
	year = {2007},
	keywords = {wind-tunnels; airplane propellers; balancing contro; quality control; dynamic behaviour; },
	abstract = {The focus of this paper is a versatile balancing procedure, developed to compensate for the asymmetries of a propeller blade's settable angle, in the range -5 to +35 . The standard balancing procedure (ISO 1940-1) was found to be inconsistent with the required quality grade, so a new balancing technique was created. A case study of propeller unbalance revealed a set of important details that must be uniquely assessed for such a complex balancing task. For the existing ISO notes, most of these details are descriptive rather than comprehensive. The new balancing concept defines the following: acceptable tolerances (shape, run-out and roughness), balancing order and priorities, a lower margin of residual unbalance, balancing accessories and regimes, unbalance correction and the verification of the results.},
	issn = {0039-2480},	pages = {319-328},	doi = {},
	url = {https://www.sv-jme.eu/sl/article/an-advanced-balancing-methodology-for-the-propeller-of-a-wind-tunnel-model/}
}

Veg, A.
2007 November 53. An Advanced Balancing Methodology for the Propeller of a Wind-Tunnel Model. Strojniški vestnik - Journal of Mechanical Engineering. [Online] 53:5

%A Veg, Aleksandar 
%D 2007
%T An Advanced Balancing Methodology for the Propeller of a Wind-Tunnel Model
%B 2007
%9 wind-tunnels; airplane propellers; balancing contro; quality control; dynamic behaviour; 
%! An Advanced Balancing Methodology for the Propeller of a Wind-Tunnel Model
%K wind-tunnels; airplane propellers; balancing contro; quality control; dynamic behaviour; 
%X The focus of this paper is a versatile balancing procedure, developed to compensate for the asymmetries of a propeller blade's settable angle, in the range -5 to +35 . The standard balancing procedure (ISO 1940-1) was found to be inconsistent with the required quality grade, so a new balancing technique was created. A case study of propeller unbalance revealed a set of important details that must be uniquely assessed for such a complex balancing task. For the existing ISO notes, most of these details are descriptive rather than comprehensive. The new balancing concept defines the following: acceptable tolerances (shape, run-out and roughness), balancing order and priorities, a lower margin of residual unbalance, balancing accessories and regimes, unbalance correction and the verification of the results.
%U https://www.sv-jme.eu/sl/article/an-advanced-balancing-methodology-for-the-propeller-of-a-wind-tunnel-model/
%0 Journal Article
%R 
%& 319
%P 10
%J Strojniški vestnik - Journal of Mechanical Engineering
%V 53
%N 5
%@ 0039-2480
%8 2017-11-03
%7 2017-11-03

Veg, Aleksandar.
"An Advanced Balancing Methodology for the Propeller of a Wind-Tunnel Model." Strojniški vestnik - Journal of Mechanical Engineering [Online], 53.5 (2007): 319-328. Web.  23 Nov. 2024

TY  - JOUR
AU  - Veg, Aleksandar 
PY  - 2007
TI  - An Advanced Balancing Methodology for the Propeller of a Wind-Tunnel Model
JF  - Strojniški vestnik - Journal of Mechanical Engineering
DO  - 
KW  - wind-tunnels; airplane propellers; balancing contro; quality control; dynamic behaviour; 
N2  - The focus of this paper is a versatile balancing procedure, developed to compensate for the asymmetries of a propeller blade's settable angle, in the range -5 to +35 . The standard balancing procedure (ISO 1940-1) was found to be inconsistent with the required quality grade, so a new balancing technique was created. A case study of propeller unbalance revealed a set of important details that must be uniquely assessed for such a complex balancing task. For the existing ISO notes, most of these details are descriptive rather than comprehensive. The new balancing concept defines the following: acceptable tolerances (shape, run-out and roughness), balancing order and priorities, a lower margin of residual unbalance, balancing accessories and regimes, unbalance correction and the verification of the results.
UR  - https://www.sv-jme.eu/sl/article/an-advanced-balancing-methodology-for-the-propeller-of-a-wind-tunnel-model/

@article{{}{.},
	author = {Veg, A.},
	title = {An Advanced Balancing Methodology for the Propeller of a Wind-Tunnel Model},
	journal = {Strojniški vestnik - Journal of Mechanical Engineering},
	volume = {53},
	number = {5},
	year = {2007},
	doi = {},
	url = {https://www.sv-jme.eu/sl/article/an-advanced-balancing-methodology-for-the-propeller-of-a-wind-tunnel-model/}
}

TY  - JOUR
AU  - Veg, Aleksandar 
PY  - 2017/11/03
TI  - An Advanced Balancing Methodology for the Propeller of a Wind-Tunnel Model
JF  - Strojniški vestnik - Journal of Mechanical Engineering; Vol 53, No 5 (2007): Strojniški vestnik - Journal of Mechanical Engineering
DO  - 
KW  - wind-tunnels, airplane propellers, balancing contro, quality control, dynamic behaviour, 
N2  - The focus of this paper is a versatile balancing procedure, developed to compensate for the asymmetries of a propeller blade's settable angle, in the range -5 to +35 . The standard balancing procedure (ISO 1940-1) was found to be inconsistent with the required quality grade, so a new balancing technique was created. A case study of propeller unbalance revealed a set of important details that must be uniquely assessed for such a complex balancing task. For the existing ISO notes, most of these details are descriptive rather than comprehensive. The new balancing concept defines the following: acceptable tolerances (shape, run-out and roughness), balancing order and priorities, a lower margin of residual unbalance, balancing accessories and regimes, unbalance correction and the verification of the results.
UR  - https://www.sv-jme.eu/sl/article/an-advanced-balancing-methodology-for-the-propeller-of-a-wind-tunnel-model/

Veg, Aleksandar"An Advanced Balancing Methodology for the Propeller of a Wind-Tunnel Model" Strojniški vestnik - Journal of Mechanical Engineering [Online], Volume 53 Number 5 (03 November 2017)