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An Analysis of the Effects of Wing Aspect Ratio and Tail Location on Static Longitudinal Stability Below the Mach Number of Lift DivergenceAn analysis is presented of the influence of wing aspect ratio and tail location on the effects of compressibility upon static longitudinal stability. The investigation showed that the use of reduced wing aspect ratios or short tail lengths leads to serious reductions in high-speed stability and the possibility of high-speed instability.
Document ID
19930085834
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
External Source(s)
hdl:100.2/ADA800674
Authors
Axelson, John A. (National Advisory Committee for Aeronautics. Ames Aeronautical Lab. Moffett Field, CA, United States)
Crown, J. Conrad (National Advisory Committee for Aeronautics. Ames Aeronautical Lab. Moffett Field, CA, United States)
Date Acquired
August 16, 2013
Publication Date
January 9, 1948
Subject Category
Aerodynamics
Report/Patent Number
NACA-RM-A7J13
Report Number: NACA-RM-A7J13
Accession Number
93R15124
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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