Method for determination of velocity and pressure distributions in subsonic range of gas with adiabatic equation of state; pressure distributions in compressible and incompressible medium compared on model problem. English translation from ZWB, Forschungsbericht n 1169-1 Jan 15 1940.
Calculation of pressure distribution on bodies of revolution in subsonic flow of gas -- I -- Axially symmetrical flow
Nat Advisory Committee Aeronautics -- Tech Memo
1947
27 pages
4 Supp Sheets
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
SUBSONIC FLOW ABOUT UNALIGNED THICK BODIES OF REVOLUTION
NTRS | 1963
|Comparison of plane and axially symmetrical flow around resistance bodies
Engineering Index Backfile | 1930
|