whereas pressure ratios greater than about two ( 2will causesupersonic flow
At the working end of the tube has one or more holes , mostly on the sides of it that supply air flows with high velocityto createturbulence in the cavity
In this manner , raising an interior wall would require a greater pressure differential between inlet 14 and outlets 16 and 18to createsupersonic flow
suflicientto causesupersonic flow within
the air 's acceleration over the airfoil(passive) caused bysupersonic flow
orderto createsupersonic flow
which is designed to converge the flow upon itselfcausingsupersonic flow
Congestion problems ... a minimum throat area 22causeplugging of the supersonic flow
which heats the material above its melting pointto createflow through the cavity
time - dependent loadingresultingfrom the supersonic cavity flow
shock waves which impinge on the subprojectile , which in turn can lead to subprojectiledisturbancecreateshock waves which impinge on the subprojectile , which in turn can lead to subprojectiledisturbance
the gas flow 30 to become subsoniccausesthe gas flow 30 to become subsonic
to a quasi - two - dimensional flowleadingto a quasi - two - dimensional flow
to research for the Atomic Energy Commission at Lawrence Livermore National Laboratoryledto research for the Atomic Energy Commission at Lawrence Livermore National Laboratory
a discontinuous shock boundary that emanates from the aircraft surface and the shock wave propagates behind the aircraft with a large amount of energycreatesa discontinuous shock boundary that emanates from the aircraft surface and the shock wave propagates behind the aircraft with a large amount of energy
in poor quality of the partresultingin poor quality of the part
on September 8thcreatedon September 8th
the temperature distribution outside of the cavity(passive) is ... influenced bythe temperature distribution outside of the cavity