发明名称 |
Flared sonic end nozzle velocity coupling test burner |
摘要 |
A flared sonic end nozzle velocity coupling test burner having a body, the walls of which define a chamber. The chamber is closed at one end thereof and has a flared sonic nozzle at the other end. Tests are performed for determining velocity coupling response with a propellant driver located adjacent to the closed end of the chamber and the propellant sample being situated during a first test at approximately the quarter length position and during the second test at approximately the three quarter length position.
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申请公布号 |
US4130011(A) |
申请公布日期 |
1978.12.19 |
申请号 |
US19770806437 |
申请日期 |
1977.06.14 |
申请人 |
THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE AIR FORCE |
发明人 |
MICHELI, PAUL L. |
分类号 |
F02K9/96;G01N25/50;G01N33/22;(IPC1-7):G01N33/22 |
主分类号 |
F02K9/96 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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