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.
Series InformationTechnical note (United States. National Advisory Committee for Aeronautics) ; 3228.
- Physical Description: 1 online resource (62 pages) : illustrations.
- Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics, 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).
Search for related items by subject
|Subject:||Angle of attack (Aerodynamics)
Propellers, Aerial > Testing.
Wind tunnel testing.