NDLI: An investigation of the aerodynamic characteristics of an 0.08-scale model of the chance vought xf7u-1 airplane in the langley high-speed 7- by 10-foot tunnel. part i - basic longitudinal stability characteristics, ted no. naca de308. part 1; basic longitudinal stability characteristics, ted no. naca de308

Content Provider	NASA Technical Reports Server (NTRS)
Copyright Year	1947
Description	The stability and control characteristics of an 0.08-scale model of the Chance Vought XF7U-1 airplane have been investigated over a Mach number range from 0.40 to 0.91. Results of the basic longitudinal tests of the complete model with undeflected control surfaces are given in the present report with a very limited analysis of the results.
File Size	9147937
Page Count	19
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_20050019437
Archival Resource Key	ark:/13960/t6vx4pr1n
Language	English
Publisher Date	1947-01-01
Access Restriction	Open
Subject Keyword	Aircraft Stability And Control Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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