Publikationsdatum:
2019-06-28
Beschreibung:
The Langley 14- by 22-Foot Subsonic Tunnel is used to test a large variety of aircraft and nonaircraft models. To support these investigations, a data acquisition system has been developed that has both static and dynamic capabilities. The static data acquisition and reduction system is described; the hardware and software of this system are explained. The theory and equations used to reduce the data obtained in the wind tunnel are presented; the computer code is not included.
Schlagwort(e):
AERODYNAMICS
Materialart:
NASA-TM-4563
,
L-17263
,
NAS 1.15:4563
Format:
application/pdf
