1991
DOI: 10.2514/4.866104
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High-Speed Flight Propulsion Systems

Abstract: ProlegomenaThe early decades of aviation were characterized by the pursuit of speed and altitude, range, and extended range at high flight speeds.A major push for higher speed was initiated by the X-series of aircraft that explored the supersonic flight regime in the 1950s and 1960s.

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Cited by 24 publications
(1 citation statement)
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“…On average, after initial variation, both can be well explained by a growth rate of S δ = 0.1. Zong and Nepf (2012) also found S δ ≈ 0.1, which is within the broad range of theoretical mixing layer spreading rates observed in previous shear layer studies S δ = α= 0.06-0.12 (Dimotakis, 1991;Marjoribanks et al, 2014;Pope, 2000;Sukhodolova & Sukhodolov, 2012). Therefore, it is justifiable to state that for rigid shoots, patches with w> 0.177 m will have height-dependent wake lengths.…”
Section: 1029/2019jf005012supporting
confidence: 83%
“…On average, after initial variation, both can be well explained by a growth rate of S δ = 0.1. Zong and Nepf (2012) also found S δ ≈ 0.1, which is within the broad range of theoretical mixing layer spreading rates observed in previous shear layer studies S δ = α= 0.06-0.12 (Dimotakis, 1991;Marjoribanks et al, 2014;Pope, 2000;Sukhodolova & Sukhodolov, 2012). Therefore, it is justifiable to state that for rigid shoots, patches with w> 0.177 m will have height-dependent wake lengths.…”
Section: 1029/2019jf005012supporting
confidence: 83%