VORTEX LIFTING AND TRANSPORTATION SYSTEM
The results of numerical research of lifting and transport system of aircraft vertical takeoff and landing, based on the use of the Magnus effect are presented. The formulas for determining its lift and thrust are obtained. The method of engineering calculation of the basic elements of the system ba...
Saved in:
Main Author: | L. V. Mihnenkov |
---|---|
Format: | Article |
Language: | Russian |
Published: |
Moscow State Technical University of Civil Aviation
2016-11-01
|
Series: | Научный вестник МГТУ ГА |
Subjects: | |
Online Access: | https://avia.mstuca.ru/jour/article/view/263 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
DETERMINATION OF THE BASIC PARAMETERS OF VTOL AIRCRAFT WITH VORTEX TYPE LIFTING-TRANSPORTING SYSTEM
by: L. V. Mikhnenkov
Published: (2016-12-01) -
ANALYSIS OF CONSEQUENCES OF FUNCTIONAL SYSTEMS REFUSALS ON TAKEOFF AND LANDING OF PLANE IL-96T
by: V. G. Kiselevich, et al.
Published: (2016-11-01) -
Structural Parameter Optimization of the Vector Bracket in a Vertical Takeoff and Landing Unmanned Aerial Vehicle
by: Wenshuai Liu, et al.
Published: (2025-05-01) -
TO THE STUDY OF WAKE VORTEX BEHIND THE AIRBUS-380 CHARACTERISTICS AT TAKEOFF AND LANDING
by: A. I. Zhelannikov
Published: (2017-01-01) -
MDO of Robotic Landing Gear Systems: A Hybrid Belt-Driven Compliant Mechanism for VTOL Drones Application
by: Masoud Kabganian, et al.
Published: (2025-06-01)