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Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails. II. Mass distributed along the fuselage / by Oscar Seidman and A.I. Neihouse.

Record details

  • Physical Description: 1 online resource (11 pages, 17 unnumbered pages) : illustrations.
  • Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics, 1937.

Content descriptions

General Note:
"December 1937."
No Federal Depository Library Program (FDLP) item number.
Bibliography, etc. Note:
Includes bibliographical references (page 11).
Source of Description Note:
Description based on online resource, PDF version; title from title page (TRAIL, viewed August 4, 2021).
Subject: Spin (Aerodynamics)
Airplanes > Fuselage.
Airplanes > Tail surfaces.
Airplanes > Wings.
Mass (Physics)
Wind tunnel testing.
Aerodynamic load.

Series Information

Technical note (United States. National Advisory Committee for Aeronautics) ; 630.

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