2002
DOI: 10.21236/ada412671
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F/A-18E/F Nacelle Simulator Input/Output Boundary Condition Flows

Abstract: Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing this collection of information. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden, to Department of Defense, Washington Headquarters Services, Directorate for Inf… Show more

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Cited by 3 publications
(6 citation statements)
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“…Air leaves the nacelle to balance inflow through several vents and openings. The relative flow through the various paths was measured and found to be independent of air-flow rate [6,20] m from the nacelle front. The remaining 25% of the air leaves through four openings in the nacelle front simulating connections to the AMAD bay and other parts of the aircraft.…”
Section: Flow Field Without Fire or Suppressant Injectionmentioning
confidence: 99%
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“…Air leaves the nacelle to balance inflow through several vents and openings. The relative flow through the various paths was measured and found to be independent of air-flow rate [6,20] m from the nacelle front. The remaining 25% of the air leaves through four openings in the nacelle front simulating connections to the AMAD bay and other parts of the aircraft.…”
Section: Flow Field Without Fire or Suppressant Injectionmentioning
confidence: 99%
“…The remaining 25% of the air leaves through four openings in the nacelle front simulating connections to the AMAD bay and other parts of the aircraft. In the ground simulator, the flow out the lower diamond vent, located directly below the upper diamond vent, is effectively zero; this may be because the fine mesh screen covering the vent was clogged with soot, rust and other particulate [6,20]. The flow rate out of the various openings was matched to the measured flow rates [6,20] by varying the porosity of the opening, given the known area of the opening.…”
Section: Flow Field Without Fire or Suppressant Injectionmentioning
confidence: 99%
“…The nominal water flow rate was 3.0 kg/h ± 0.35 kg/h at a line pressure immediately upstream of the atomizer of 791 kPa ± 65 kPa. 2 The pressure was held constant for the two HFE agents so that liquid atomization would be comparable (thus the flow rates varied according to the change in liquid density; see Table 1). Characterization of the atomizer was only carried out to the extent of providing initial conditions for the modeling effort; data are reported in Appendix A.…”
Section: Experimental Arrangementmentioning
confidence: 99%
“…A high-resolution digital camera provided still images and movies (at 9 frames/s) of the spray. A high-speed digital camera (at 1000 frames/s) [23,24] was used to record the 2 Estimation of the measurement uncertainty is determined from statistical analysis of a series of replicated measurements (referred to as a type A evaluation of uncertainty) and from other means other than statistical analysis (referred to as a type B evaluation of uncertainty) [33], calculated as 2u c (representing a level of confidence of 95 %), where u c is the combined standard uncertainty. The value for u c was estimated statistically by sn -1/2 , where s is the standard deviation of the mean and n is the number of samples (type A uncertainty, where n = 11) and from the manufacturer uncertainty (type B uncertainty), if available.…”
Section: Experimental Arrangementmentioning
confidence: 99%
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