Accession Number:

ADA089377

Title:

An Introduction to Dynamic Derivatives (3) Methods of Oscillating Models in Pitch and Yaw in a 530 by 810 Millimetre Transonic Wind Tunnel.

Descriptive Note:

Aerodynamics note,

Corporate Author:

AERONAUTICAL RESEARCH LABS MELBOURNE (AUSTRALIA)

Personal Author(s):

Report Date:

1979-04-01

Pagination or Media Count:

49.0

Abstract:

Mechanisms are considered which allow models to be oscillated in pitch and yaw during wind tunnel tests to measure dynamic derivatives. Types of pivots, motion producing linkages and connecting linkages are described as applicable in a 530 by 810 millimeter Transonic Tunnel. Author

Subject Categories:

  • Test Facilities, Equipment and Methods

Distribution Statement:

APPROVED FOR PUBLIC RELEASE