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Rocket-model investigation of the longitudinal stability, drag, and duct performance of a 60 deg delta wing canard aircraft with twin side inlets at Mach numbers from 0.80 to 1.70
Document ID
19690067239
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Bond, A. C. (NASA Langley Research Center Hampton, VA, United States)
Swanson, A. G. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 5, 2013
Publication Date
March 29, 1954
Publication Information
Publisher: NACA
Subject Category
Unknown
Report/Patent Number
NACA-RM-L53D10A
Accession Number
69N71418
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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