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Wind Tunnel Investigation at Low Speed of Aerodynamic Characteristics of Army Chemical Corps Model E-112 Bomblets with Span Chord Ratio of 2 - 1An experimental investigation has been made in the Langley stability tunnel to determine the aerodynamic characteristics of the Army Chemical Corps model E-112 bomblets with span-chord ratio of 2:1. A detailed analysis has not been made; however, the results showed that all the models were spirally unstable and that a large gap between the model tips and end plates tended to reduce the instability.
Document ID
19710074594
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Letko, W. (National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
August 6, 2013
Publication Date
December 26, 1956
Subject Category
Aerodynamics
Report/Patent Number
NACA-RM-SL56L20
Report Number: NACA-RM-SL56L20
Accession Number
71X73176
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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