Accession Number:

AD0848019

Title:

Model 8-82 Wing-Tip Deflection Test,

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS SAN DIEGO CA CONVAIR DIV

Personal Author(s):

Report Date:

1954-06-03

Pagination or Media Count:

48.0

Abstract:

The report describes results obtained from applied loading of the wing surfaces of an F-102 aircraft.

Subject Categories:

  • Attack and Fighter Aircraft
  • Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE