A transonic wind-tunnel investigation of the longitudinal force and moment characteristics of two delta wings and one clipped-tip delta wing of 4 percent thickness on a slender body

Author: Palmer, William E.
Additional Authors: Burrows, Dale L.
Year: 1955
Document Type: MAIN
SUDOC: Y 3.N21/5:15/L55A07a
Series: NACA research memorandum ;
Report Number: L55A07a
Subjects: Stability of airplanes, Longitudinal
Delta wing airplanes--Handling characteristics
Link: https://hdl.handle.net/2027/mdp.39015095100866

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