PRELIMINARY REPORT OF PHASE IV OF THE AERODYNAMIC HEATING TEST AT THE NASA LANGLEY UNITARY PLAN WIND TUNNEL,
Abstract
This is a preliminary test report for an aerodynamic heating test of guided missile protuberances.
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 01, 1959
- Accession Number
- AD0834045
Entities
People
- P. S. Yip
Organizations
- General Dynamics