Aerodynamic characteristics of Goodyear-Zeppelin airship models at tank pressures varying from 1 to 20 atmos.; range of Reynolds Number about 1,000,000 to 40,000,000; addition of fins and car to bare hull of model causes increase in lift at positive angles of pitch; little change in drag coefficient between fineness ratio of about five and seven; effect of surface roughness very large.
Airship model tests in the variable density wind tunnel
Nat. Advisory Committee Aeronautics -- Report
1931
24 pages
28 Figs.
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Airship Model Tests in the Variable Density Wind Tunnel
NTRS | 1932
|Airship model test in the variable density wind tunnel
TIBKAT | 1931
|