2022
DOI: 10.34759/vst-2022-2-45-60
|View full text |Cite
|
Sign up to set email alerts
|

Studying Dependence of “Rigid” Aerodynamic Models Elastic Deformations on Their Geometric and Design Parameters

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1

Citation Types

0
1
0

Year Published

2023
2023
2023
2023

Publication Types

Select...
1

Relationship

0
1

Authors

Journals

citations
Cited by 1 publication
(1 citation statement)
references
References 0 publications
0
1
0
Order By: Relevance
“…With an increase in the moment of inertia of the model, the function of the dependence of the aerodynamic moment on the angle of attack acquires rectilinear sections, while the time of the transition process increases (Fig. 4, 5) [10]. In this case, the motion of the aircraft is significantly affected by the inertial properties of the object itself.…”
Section: Research Of the Influence Of The Results Obtained In The Exp...mentioning
confidence: 95%
“…With an increase in the moment of inertia of the model, the function of the dependence of the aerodynamic moment on the angle of attack acquires rectilinear sections, while the time of the transition process increases (Fig. 4, 5) [10]. In this case, the motion of the aircraft is significantly affected by the inertial properties of the object itself.…”
Section: Research Of the Influence Of The Results Obtained In The Exp...mentioning
confidence: 95%