Mathematical analysis of airflow conditions and pressure distribution based on shape of ZR 111, with following simplifications: cars, fins and rudders removed; all cross sections replaced by equivalent circular cross sections; calculations are made for symmetrical case, of flow parallel to axis; unsymmetrical case, or flow at angle to axis.
Calculation of pressure distribution on airship hulls
Nat. Advisory Committee Aeronautics -- Tech. Memorandum
1930
27 pages
9 Figs.
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Calculation of Pressure Distribution on Airship Hulls
NTRS | 1930
|AIAA | 1977
|Stability equations for airship hulls
TIBKAT | 1925
|Stability equations for airship hulls
Engineering Index Backfile | 1925
|Stability equations for airship hulls
NTRS | 1926
|