Model 8-82 Wing-Tip Deflection Test,
Abstract
The report describes results obtained from applied loading of the wing surfaces of an F-102 aircraft.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 03, 1954
- Accession Number
- AD0848019
Entities
People
- R. J. Haney
- W. E. Wise
Organizations
- General Dynamics