A performance analysis of methods for handling excess inlet flow at supersonic speeds / Donald P. Hearth and James F. Connors.
A comparison was made of several methods far handling excess inlet flow for the Mach number range from 1.5 to 4.0. The following techniques were examined and evaluated in terms of their respective thrust penalties for an assumed turbojet engine: normal- and olique-shock spillage, bypassing through a...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington :
National Advisory Committee for Aeronautics,
[1958]
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
4270. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/4270
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| Y 3.N 21/5:6/4270 | Available Place a Hold |