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.
Series InformationTechnical note (United States. National Advisory Committee for Aeronautics) ; 310.
- Physical Description: 1 online resource (13 pages, 20 unnumbered pages) : illustrations.
- Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics, 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).
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|Subject:||Airplanes > Wings > Design and construction.
Wind tunnel testing.