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Wind tunnel pressure distribution tests on a series of biplane wing models. Part I. Effects of changes in stagger and gap / by Montgomery Knight and Richard W. Noyes.

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Record details

  • Physical Description: 1 online resource (13 pages, 20 unnumbered pages) : illustrations.
  • Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics, 1929.

Content descriptions

General Note:
"July, 1929."
No Federal Depository Library Program (FDLP) item number.
Bibliography, etc. Note:
Includes bibliographical references (page 13).
Source of Description Note:
Description based on online resource, PDF version; title from title page (TRAIL, viewed August 18, 2020).
Subject: Airplanes > Wings > Design and construction.
Wind tunnel testing.

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