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Aerodynamic investigation of a four-blade propeller operating through an angle-of-attack range from 0° to 180° / by H. Clyde McLemore and Michael D. Cannon.

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Record details

  • Physical Description: 1 online resource (62 pages) : illustrations.
  • Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics, 1954.

Content descriptions

General Note:
"June 1954."
No Federal Depository Library Program (FDLP) item number.
Bibliography, etc. Note:
Includes bibliographical references (page 15).
Source of Description Note:
Description based on online resource, PDF version; title from title page (TRAIL, viewed August 5, 2020).
Subject: Angle of attack (Aerodynamics)
Mathematical analysis.
Propellers, Aerial > Testing.
Wind tunnel testing.

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