Aircraft Design, Systems and Technology Meeting 1983
DOI: 10.2514/6.1983-2527
|View full text |Cite
|
Sign up to set email alerts
|

NOTAR - The viable alternative to a tail rotor

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1
1

Citation Types

0
6
0

Year Published

2009
2009
2023
2023

Publication Types

Select...
3
2
1

Relationship

0
6

Authors

Journals

citations
Cited by 6 publications
(6 citation statements)
references
References 0 publications
0
6
0
Order By: Relevance
“…10. Table 2 Contrast between calculation data and experimental data The variation tendency of lateral force coefficient Cy with momentum coefficient Cμ was same as experimental data [1]. With the increase of Cμ, the lateral force coefficient Cy increased gradually.…”
Section: Model Validation and Analysismentioning
confidence: 63%
See 2 more Smart Citations
“…10. Table 2 Contrast between calculation data and experimental data The variation tendency of lateral force coefficient Cy with momentum coefficient Cμ was same as experimental data [1]. With the increase of Cμ, the lateral force coefficient Cy increased gradually.…”
Section: Model Validation and Analysismentioning
confidence: 63%
“…In order to validate the calculation model proposed in this paper, a three-dimensional model of anti-torque system was built according to [1], shown in Fig. 5.…”
Section: Geometry Modelmentioning
confidence: 99%
See 1 more Smart Citation
“…An illustration of that design is given in Figure 3. The absence of a tail rotor permits a better safety and reduces the noise produced by the helicopter as discussed by Sampatacos et al [14], unfortunately this comes at the cost of an increased complexity.…”
Section: Applicationsmentioning
confidence: 99%
“…This strategy has been utilized on the McDonnell Douglas NOTAR™ anti-torque system seen on the MD520N series of helicopters (Sampatacos et al, 1983). This strategy has been utilized on the McDonnell Douglas NOTAR™ anti-torque system seen on the MD520N series of helicopters (Sampatacos et al, 1983).…”
Section: Introductionmentioning
confidence: 99%