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Free-flight Investigation to Determine Some Effects of Tail Damping and Wing-tail Interference on the Rolling Effectiveness of Ailerons and a Spoiler on a Modified-delta Wing at Mach Numbers from 0.6 to 1.5
- Publication Year :
- 1957
- Publisher :
- United States: NASA Center for Aerospace Information (CASI), 1957.
Details
- Language :
- English
- Database :
- NASA Technical Reports
- Publication Type :
- Report
- Accession number :
- edsnas.19930089655
- Document Type :
- Report