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Accession Number:
AD0670594
Title:
EFFECT OF MIXING LENGTH ON ROTARY FLOW INDUCTORS,
Corporate Author:
NAVAL AIR PROPULSION TEST CENTER TRENTON N J AERONAUTICAL TURBINE DEPT
Report Date:
1968-04-01
Abstract:
A series of model tests were run using a variety of shroud configurations to determine the effect of primary-secondary flow mixing lengths on rotary nozzle ejectors. Maximum augmentation was achieved at mixing lengths of 3.5 to 4.0, whereas, non-rotating ejectors require mixing lengths of 6 to 10. Author
Pages:
0032
File Size:
0.00MB
