Accession Number:

ADA551706

Title:

X-HALE: A Very Flexible UAV for Nonlinear Aeroelastic Tests

Descriptive Note:

Conference paper

Corporate Author:

MICHIGAN UNIV ANN ARBOR DEPT OF AEROSPACE ENGINEERING

Report Date:

2010-04-01

Pagination or Media Count:

24.0

Abstract:

The University of Michigan has designed and is currently building an unmanned aerial vehicle, denoted X-HALE, which is aeroelastically representative of very flexible aircraft. The objective of this test bed is to collect unique data of the geometrically nonlinear aeroelastic response coupled with the flight dynamics to be used for future code validation. The aircraft will present specific aeroelastic features e.g., coupled rigidelastic body instability, large wing deflection during gust, etc. that can be measured in flight. Moreover, the airframe construction choice is such that the elastic, inertial and geometric properties can be well characterized. These are requirements driven by the need of the collected data to be used to support validation of coupled nonlinear aeroelasticflight dynamics codes.

Subject Categories:

  • Pilotless Aircraft
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE