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Aerodynamic characteristic of a swept-wing cruise missile at Mach numbers from 0.50 to 2.86An investigation has been made in the Mach number range from 0.50 to 2.86 to determine the longitudinal and lateral aerodynamic characteristics of a cruise missile having a 58 deg swept wing and conventional aft tails. Such a vehicle might be applicable to missions such as surface- or air-launched tactical or strategic missiles, unmanned reconnaissance, or countermeasure decoys.
Document ID
19730001275
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Spearman, M. L. (NASA Langley Research Center Hampton, VA, United States)
Collins, I. K. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1972
Subject Category
Aerodynamics
Report/Patent Number
L-8508
NASA-TN-D-7069
Accession Number
73N10002
Funding Number(s)
PROJECT: RTOP 760-67-81-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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