Transonic flutter study of a 50.5̊ cropped-delta wing with two rearward-mounted nacelles / by Maynard C. Sandford, Charles L. Ruhlin, and Irving Abel.

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Bibliographic Details
Online Access:	Search for the full-text version of this title in HathiTrust
Main Author:	Sandford, M. C. (Maynard C.)
Corporate Authors:	Langley Research Center, United States. National Aeronautics and Space Administration
Other Authors:	Ruhlin, Charles L., Abel, Irving
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1974.
Series:	NASA technical note ; D-7544.
Subjects:	Flutter (Aerodynamics) Airplanes > Nacelles. Airplanes > Wings, Triangular. Aerodynamics, Transonic.

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Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.14:D-7544
NAS 1.14:D-7544	Available Place a Hold