Accession Number:

ADA243004

Title:

Wind Loads on a Mirage III O Aircraft Mounted above a Ground Plane

Descriptive Note:

Technical memorandum,

Corporate Author:

AERONAUTICAL RESEARCH LABS MELBOURNE (AUSTRALIA)

Personal Author(s):

• Hermsen, P. A.

Report Date:

1991-08-01

Pagination or Media Count:

21.0

Abstract:

Measurements were made in ARL Salisburys Low Speed Tunnel on a 172 scale model of a Mirage III O aircraft to determine steady wind loads when mounted above a ground plane. The six component data cover 360 deg in azimuth, and roll and pitch angles of -20 deg, O deg, 20 deg.

Descriptors:

• *ANGLES
• LOW VELOCITY
• TUNNELS
• GROUND LEVEL
• PITCH(INCLINATION)

Subject Categories:

• Aerodynamics
• Attack and Fighter Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE