Analysis of a spin and recovery from time histories of attitudes and velocities as determined for a dynamic model of a contemporary fighter airplane in the free-spinning tunnel / by Stanley H. Scher.
Series InformationTechnical note (United States. National Advisory Committee for Aeronautics) ; 3611.
- Physical Description: 1 online resource (54 pages) : illustrations.
- Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics, 1956.
No Federal Depository Library Program (FDLP) item number.
|Bibliography, etc. Note:||
Includes bibliographical references (page 22).
|Source of Description Note:||
Description based on online resource, PDF version; title from title page (TRAIL, viewed August 12, 2020).
Search for related items by subject
|Subject:||Airplanes > Testing.
Wind tunnel testing.