Acceleration of high-pressure-ratio single-spool turbojet engine as determined from component performance characteristics III : effect of turbine stator adjustment

Creator(s):
Creation Date: August 2, 1954
Partner(s):
UNT Libraries Government Documents Department
Collection(s):
National Advisory Committee for Aeronautics Collection
Technical Report Archive and Image Library
Usage:
Total Uses: 240
Past 30 days: 2
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Creator (Author):
Creator (Author):
Date(s):
  • Creation: August 2, 1954
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Contributor(s):
Serial Title: NACA Research Memorandums
Partner:
UNT Libraries Government Documents Department
Collection:
National Advisory Committee for Aeronautics Collection
Collection:
Technical Report Archive and Image Library
Identifier:
  • : 93R17492
  • URL: http://hdl.handle.net/2060/19930088202
  • REP-NO: NACA-RM-E54F04
  • CASI: 19930088202
  • ARK: ark:/67531/metadc60396
Resource Type: Report
Format: Text
Rights:
Access: Public
Statement: No Copyright, Unclassified, Unlimited, Publicly available