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Accession Number:
AD0249771
Title:
STRUCTURAL TEST PROGRAM F-106A AIRPLANE
Corporate Author:
WRIGHT AIR DEVELOPMENT DIV WRIGHT-PATTERSON AFB OH ENGINEERING TEST DIV
Report Date:
1960-08-01
Abstract:
The F-106 airplane was subjected to a complete static test program covering all of the critical flight, landing and ground handling conditions.
Supplementary Note:
DOI: 10.21236/AD0249771
Pages:
0072
Distribution Statement:
Approved for public release; distribution is unlimited. Document partially illegible.
File Size:
3.87MB
