Development of tunnel in which test Mach numbers from 0.6 to slightly over 1.0 are achieved by rotating test model in annular passage between two concentric cylinders. Supersedes declassified NACA RM L8A23, Rm L50E18, and RM L9G19.
Langley annular transonic tunnel
NACA -- Report
1952
10 pages
Report
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
The Langley Annular Transonic Tunnel
NTRS | 1952
|The Langley annular transonic tunnel
TIBKAT | 1952
|Rotorcraft aeroelastic testing in the Langley Transonic Dynamics Tunnel
Tema Archiv | 1993
|