Effect of Nose Slenderness on Forebody Flow Control

Effect of Nose Slenderness on Forebody Flow Control

When attempting to transfer the forebody flow control technology developed on military aircraft to commercial aircraft, such as the Boeing 1804 SST, additional flow parameters become important. The reason for the complication of the technology transfer is the large difference in forebody slenderness...

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Bibliographische Detailangaben
Veröffentlicht in:Journal of aircraft 1999-09, Vol.36 (5), p.885-889
Hauptverfasser: Ericsson, Lars E, Beyers, Martin E
Format: Artikel
Sprache:eng
Schlagworte:
Air transportation and traffic
Applied sciences
Exact sciences and technology
Ground, air and sea transportation, marine construction
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Beschreibung
Zusammenfassung:When attempting to transfer the forebody flow control technology developed on military aircraft to commercial aircraft, such as the Boeing 1804 SST, additional flow parameters become important. The reason for the complication of the technology transfer is the large difference in forebody slenderness, with apex half-angles below 10 deg in the commercial case compared to above 25 deg for military aircraft. Available experimental results are interpreted on the basis of the existing database for bodies of revolution. (Author)
ISSN:0021-8669
1533-3868
DOI:10.2514/2.2522