CALCULATION OF THE FORCE COEFFICIENT FOR DELTA WINGS IN HYPERSONIC FLOW.
Abstract
The results of the Newtonian theory as applied to a delta wing at moderate angles of attack in hypersonic stream are used to calculate the pressure coefficient by the inverse method in a closed form. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1965
- Accession Number
- AD0625404
Entities
People
- Arnold Polak
Organizations
- University of Cincinnati