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Longitudinal aerodynamic characteristics of a 1/30-scale subsonic canard-airplane model having a wing with an aspect ratio of 3.6 at mach numbers from 0.30 to 0.98Wind tunnel aerodynamic characteristics of subsonic nuclear powered canard aircraft model
Document ID
19650017036
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Capone, F. J. (NASA Langley Research Center Hampton, VA, United States)
Igoe, W. B. (NASA Langley Research Center Hampton, VA, United States)
Re, R. J. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1962
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-669
Accession Number
65N26637
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
NUCLEAR AIRCRAFT
AERODYNAMIC CHARACTERISTICS
WIND TUNNEL
CANARD

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