A remotely controlled wind tunnel model for the demonstration of aircraft stability and control characteristics.
Main Author: | Merrill, John Christian |
---|---|
Language: | en_US |
Published: |
Monterey, California. Naval Postgraduate School
2012
|
Online Access: | http://hdl.handle.net/10945/21018 |
Similar Items
-
The design development and evaluation of an active control aircraft model wind tunnel facility
by: Malik, I. A.
Published: (1982) -
Wind Tunnel Modelling of Aerodynamic Baffle Arrays for Aircraft Exhaust Plume Control
by: Velikov, S.
Published: (2015) -
Wind tunnel modelling of aerodynamic baffle arrays for aircraft exhaust plume control
by: Velikov, S.
Published: (2014) -
Control of a wind tunnel manoeuvre-rig to physically simulate free-flight motion of an aircraft model
by: Araujo-Estrada, Sergio A.
Published: (2016) -
A Wind Tunnel Testing on the Aerodynamics Characteristic of an Unmanned Joined-wing Aircraft
by: Chun-Jen Lin, et al.
Published: (2006)