1999
DOI: 10.1017/s0001924000065064
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Unsteady aerodynamics: retrospect and prospect

Abstract: This paper reviews some current problems in unsteady aerodynamics and discusses some future challenges. The emphasis is on problems associated with separated flows, such as buffeting and limit cycle oscillations. Suggestions are made to indicate how experimental facilities (such as cryogenic windtunnels) and computational fluid dynamics might be exploited to address these questions.

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Cited by 12 publications
(4 citation statements)
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“…Bruce). buffet phenomenon [8,9], while in transonic diffusers, disturbances generated in the boundary layer downstream of the interaction region have been linked to large-scale unsteady shock motion [7,12]. In contrast, disturbances that originate upstream of transonic interactions have been found to produce shock unsteadiness of a somewhat smaller scale that is often of less concern.…”
Section: Introductionmentioning
confidence: 99%
“…Bruce). buffet phenomenon [8,9], while in transonic diffusers, disturbances generated in the boundary layer downstream of the interaction region have been linked to large-scale unsteady shock motion [7,12]. In contrast, disturbances that originate upstream of transonic interactions have been found to produce shock unsteadiness of a somewhat smaller scale that is often of less concern.…”
Section: Introductionmentioning
confidence: 99%
“…Unsteady flows are encountered in many aerospace applications and prediction of unsteady air loads plays a vital role in aircraft and helicopter design (Mabey, 1999;McCroskey 1982;McCroskey, W. J. 1988).…”
Section: Introductionmentioning
confidence: 99%
“…In many cases, dynamic stall becomes primary limiting factor in the performance of the associated vehicle or structure. Unsteady flows are encountered in many aerospace applications and prediction of unsteady air loads plays a vital role in aircraft and helicopter design [1][2][3]. Since wind tunnel testing of unsteady flow situations is difficult and expensive, computational studies of wing stall, dynamic stall, blade-vortex interaction of helicopter rotors and aeroelastic problems like flutter, buffeting and gust-response etc., can provide important design data.…”
Section: Introductionmentioning
confidence: 99%