Simulator investigations of non-maneuverable aircraft reaching high angles of attack in a controlled way
In-flight experiments are considered the most appropriate means to simplify the development of mathematical models of transport-type aircraft aerodynamic characteristics, which take into account the dynamics of forces and moments arising over a wide range of angles of attack up to the highest ones....
Saved in:
Main Author: | P. L. Sverkanov |
---|---|
Format: | Article |
Language: | Russian |
Published: |
Moscow State Technical University of Civil Aviation
2025-07-01
|
Series: | Научный вестник МГТУ ГА |
Subjects: | |
Online Access: | https://avia.mstuca.ru/jour/article/view/2581 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
RESEARCH OF AERODYNAMIC CHARACTERISTICS OF THE MODEL OF MANEUVERABLE AIRCRAFT WITH MECHANIZED LEADING EDGE USING SOFTWARE ANSYS FLUENT
by: A. V. Golovnev, et al.
Published: (2016-11-01) -
Study on correction technology of aircraft angle-of-attack signal based on estimation of side-slip angle
by: XUE Yuan, et al.
Published: (2025-06-01) -
CONDITIONS FOR SAFETY OPERATION AND MANEUVERABILITY OF LOW-TONNAGE ROADTRAIN AT CRITICAL RATES OF MOTION
by: Z. A. Godzhaev, et al.
Published: (2017-12-01) -
Pectoral Fin-Assisted Braking and Agile Turning: A Biomimetic Approach to Improve Underwater Robot Maneuverability
by: Qu He, et al.
Published: (2025-06-01) -
MATHEMATICAL MODEL OF THE MOTION OF A LIGHT ATTACK AIRCRAFT WITH EXTERNAL LOAD SLINGS IN THE EXTREME AREA OF FLIGHT MODES ACCORDING TO THE ANGLE OF ATTACK
by: S. A. Popov, et al.
Published: (2017-05-01)