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Advanced Technology Thrust Vectoring Exhaust Systems

Authors: J. GILL;

Advanced Technology Thrust Vectoring Exhaust Systems

Abstract

Figures 18-21 are plots of some data recorded during the flight tests. These data are typical of the flight test data and are included to show the similarity with the laboratory data. These plots cannot be compared directly with any of the other data presented here for the same reasons given in the paragraph on drop tests. They do show, however, that similar data is obtained from the three test methods (roller plate platforms, shuttle plate, and flight test) so long as there is no requirement for running over deck obstructions. When this requirement is present, the shuttle plate provides the better and more economical method. Conclusions

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selected citations
These citations are derived from selected sources.
This is an alternative to the "Influence" indicator, which also reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
BIP!Citations provided by BIP!
popularity
This indicator reflects the "current" impact/attention (the "hype") of an article in the research community at large, based on the underlying citation network.
BIP!Popularity provided by BIP!
influence
This indicator reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
BIP!Influence provided by BIP!
impulse
This indicator reflects the initial momentum of an article directly after its publication, based on the underlying citation network.
BIP!Impulse provided by BIP!
5
Average
Top 10%
Top 10%
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