Remarks About Rp Frasers Reports On Jet Research
Remarks About Rp Frasers Reports On Jet Research
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) Whether or not the occurrence of shocks is mainly responsible for the devr'ation from theoretical expecta- tion is still the question. Fraser himself gives a differ- ent explanation: "At 15° and greater divergences it may be tht t the frictional loss in the convergent portion is the more important pert. This causes a consequent drop in the pressure at the throf^. T to below the theoretical critical pressure nnd, therefore, a consequent drop in the pressures along the divergence. The rising mo...uth pressure with increasing divergence must then be attributed to a further departure from the adiabatic expansion in the divergence due to general turbulence rather than wall fric- tion. " Eraser's argument would also hold for nozzles with a smooth throat. It would, therefore, be of interest 'to have experimental evidence about the i erformance of smooth nozzles with wide divergence.
The preceding remarks refer to the pressure at the wall. The flow distribution over the cross-section is certainly influenced considerably by the shock fronts.
What to read after Remarks About Rp Frasers Reports On Jet Research?
You can find similar books in the "Read Also" column, or choose other free books by Kurt Otto Friedrichs to read onlineMoreLess
To quickly assess the difficulty of the text, read a short excerpt:
) Whether or not the occurrence of shocks is mainly responsible for the devr'ation from theoretical expecta- tion is still the question. Fraser himself gives a differ- ent explanation: "At 15° and greater divergences it may be tht t the frictional loss in the convergent portion is the more important pert. This causes a consequent drop in the pressure at the throf^. T to below the theoretical critical pressure nnd, therefore, a consequent drop in the pressures along the divergence. The rising mo...uth pressure with increasing divergence must then be attributed to a further departure from the adiabatic expansion in the divergence due to general turbulence rather than wall fric- tion. " Eraser's argument would also hold for nozzles with a smooth throat. It would, therefore, be of interest 'to have experimental evidence about the i erformance of smooth nozzles with wide divergence.
The preceding remarks refer to the pressure at the wall. The flow distribution over the cross-section is certainly influenced considerably by the shock fronts.
What to read after Remarks About Rp Frasers Reports On Jet Research?
You can find similar books in the "Read Also" column, or choose other free books by Kurt Otto Friedrichs to read onlineMoreLess
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