Publikationsdatum:
2013-08-31
Beschreibung:
Models featuring the simulation of exhaust jets were developed for magnetic levitation in a wind tunnel. The exhaust gas was stored internally producing a discharge of sufficient duration to allow nominal steady state to be reached. The gas was stored in the form of compressed gas or a solid rocket propellant. Testing was performed with the levitated models although deficiencies prevented the detection of jet-induced aerodynamic effects. Difficulties with data reduction led to the development of a new force calibration technique, used in conjunction with an exhaust simulator and also in separate high incidence aerodynamic tests.
Schlagwort(e):
AERODYNAMICS
Materialart:
NASA. Langley Research Center, Second International Symposium on Magnetic Suspension Technology, Part 1; p 291-305
Format:
application/pdf
