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Formation flying benefits based on vortex lattice calculationsA quadrilateral vortex-lattice method was applied to a formation of three wings to calculate force and moment data for use in estimating potential benefits of flying aircraft in formation on extended range missions, and of anticipating the control problems which may exist. The investigation led to two types of formation having virtually the same overall benefits for the formation as a whole, i.e., a V or echelon formation and a double row formation (with two staggered rows of aircraft). These formations have unequal savings on aircraft within the formation, but this allows large longitudinal spacings between aircraft which is preferable to the small spacing required in formations having equal benefits for all aircraft. A reasonable trade-off between a practical formation size and range benefit seems to lie at about three to five aircraft with corresponding maximum potential range increases of about 46 percent to 67 percent. At this time it is not known what fraction of this potential range increase is achievable in practice.
Document ID
19770013076
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Maskew, B.
(Analytical Methods, Inc. Bellevue, WA, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1977
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-151974
Report Number: NASA-CR-151974
Accession Number
77N20020
Funding Number(s)
CONTRACT_GRANT: NASA ORDER A-26151-B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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