NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Wind-tunnel and flight-test investigation of the exdrone remotely piloted vehicle configurationAt the request of the United States Marine Corps, an exploratory wind-tunnel and flight test investigation was conducted by the NASA Langley Research Center to improve the stability, controllability, and general flight characteristics of the Marine Corps Exdrone RPV (Remotely Piloted Vehicle) configuration. Static wind tunnel tests were conducted to identify and improve the stability and control characteristics of the vehicle. The wind-tunnel test resulted in several configuration modifications which included increased elevator area, increased vertical tail area and moment arm, increased rudder area and aileron area, the addition of vertical wing-tip fins, and the addition of leading-edge droops on the outboard wing panel to improve the stall departure resistance. Flight tests of the modified configuration were conducted at the NASA Plum Tree Test Site to provide a qualitative evaluation of the flight characteristics of the modified configuration.
Document ID
19900046836
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Yip, Long P.
(NASA Langley Research Center Hampton, VA, United States)
Fratello, David J.
(NASA Langley Research Center Hampton, VA, United States)
Robelen, David B.
(NASA Langley Research Center Hampton, VA, United States)
Makowiec, George M.
(Vigyan Research Associates, Inc. Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 90-1261
Meeting Information
Meeting: AIAA/SFTE/DGLR/SETP Biannual Flight Test Conference
Location: Ontario, CA
Country: United States
Start Date: May 22, 1990
End Date: May 24, 1990
Accession Number
90A33891
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available