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Deflection of delta wings having a carry-through-bay chord smaller than the wing root chord
- Author / Creator
- Available as
- Online
- Summary
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Experimenatally determined influence coefficients are presented for the deflection of two solid delta wings - one wing of constant thickness and the other of constant thickness ratio - having a car...
Experimenatally determined influence coefficients are presented for the deflection of two solid delta wings - one wing of constant thickness and the other of constant thickness ratio - having a carry-through-bay chord smaller than the wing root chord. A theoretical method of analysis is demonstrated for the constant-thickness wing under tip load, and the theoretical results are compared with the experimental results. The theoretical tip-load deflection for a constant-thickness delta wing elastically supported by a carry-through bay of width 35 percent of the wing root chord is twice as large at the tip as the theoretical tip-load deflection for a similar wing clamped 100 percent of the chord at the root.
Details
- Creator
- by Roger W. Peters and Manuel Stein
- Format
- Books
- Language
- English
- Contributors
- Publication
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- Washington, D.C. : National Advisory Committee for Aeronautics, 1953
- Physical Details
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- 1 online resource (25 pages) : illustrations, tables, photographs
- data file
- OCLC
- on1371666518
- Title from title screen (viewed February 24, 2023)
- Date of issue: May 1953.
- Report no. NACA-TN-2927.
- "Langley Aeronautical Laboratory."
- Includes bibliographical references (page 15)
- Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.