Transonic Flight Tests to Compare the Zero-Lift Drags of 45 Degree Sweptback Wings of Aspect Ratio 3.55 and 6.0 With and Without Nacelles at the Wing Tips

Author: Hoffman, Sherwood
Year: 1952
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L51L27
Link: https://digital.library.unt.edu/ark:/67531/metadc59128/

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