Helicopter Remote Wind Sensor Flight Test.
Abstract
A flight test program has been completed in which the Helicopter Remote Wind Sensor was mounted on a UH-1 testbed aircraft. Wind measurements were made and recorded under a variety of flight hover conditions. Data from the flight test program are presented as wind profiles as a function of range, and data reduction and analysis approaches are discussed. The point-pair method was applied for comparison to theoretical and wind tunnel results. The data are applied to a baseline ballistics study sufficient to estimate the quantity of data needed for free-flight aerial armaments. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 01, 1980
- Accession Number
- ADA082770
Entities
People
- David H. Dickson
- Jon E. Ottesen
Organizations
- Atmospheric Sciences Laboratory