Effect of a Lateral Support Strut on Body Pressure Distributions at Transonic Speeds,
Abstract
The effect of a strut support on the measured pressure distributions along a missile at transonic speeds was determined qualitatively by comparing data obtained on strut and sting mounts, using the same model in various configurations. The comparison showed how the presence of a mounting strut influences the pressure distribution along the model body. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1972
- Accession Number
- AD0743178
Entities
People
- Donald V. Rubin
Organizations
- United States Army Aviation and Missile Command