Airfoil measurements that show behavior of wing sections in low-turbulence stream in Reynolds number range from 20,000 to 170,000
Aerodynamics of the model airplane. Part 1 - Airfoil measurements
01.11.1967
Report
Keine Angabe
Englisch
SLUB | 1951
|Engineering Index Backfile | 1951
|Aerodynamics : Airplane design
TIBKAT | 1927
|