Development of a Technique and Method of Testing Aircraft Models with Turboprop Engine Simulators in a Small-scale Wind Tunnel - Results of Tests
This report presents the results of experimental investigations into the interaction between the propellers (Ps) and the airframe of a twin-engine, twin-boom light transport aircraft with a Π-shaped tail. An analysis was performed of the forces and moments acting on the aircraft with rotating Ps. Th...
Main Authors: | A. V. Petrov, Y. G. Stepanov, M. V. Shmakov |
---|---|
Format: | Article |
Language: | English |
Published: |
CTU Central Library
2004-01-01
|
Series: | Acta Polytechnica |
Subjects: | |
Online Access: | https://ojs.cvut.cz/ojs/index.php/ap/article/view/530 |
Similar Items
-
AN AIRPLANE WITH UNCONVENTIONALLY PLACED PROPELLER POWER UNIT
by: Jan Červinka, et al.
Published: (2017-02-01) -
Experimental Assessment of Aero-Propulsive Effects on a Large Turboprop Aircraft with Rear-Engine Installation
by: Salvatore Corcione, et al.
Published: (2023-01-01) -
Numerical Simulations Study on the Effect of Propeller Slipstream on Inlet Flow Field for a Turboprop Aircraft
by: WANG Limin, et al.
Published: (2020-06-01) -
Design, Analysis, and Testing of a Scaled Propeller for an Innovative Regional Turboprop Aircraft
by: Danilo Ciliberti, et al.
Published: (2022-05-01) -
Research on Aerodynamic Shape Design Scheme of a Distributed Propeller Transport Aircraft and Its Slipstream Effect
Published: (2019-04-01)