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.
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
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