1993
DOI: 10.2514/3.46401
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Lateral aerodynamic interference between tanker and receiver in air-to-air refueling

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Cited by 37 publications
(11 citation statements)
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“…In 1975, Jewell and Stapleford [10] and Rossow et al [18] proposed a mathematical model to describe the effect of wake. Modeling and analysis of the effect of a tanker's wake on a receiver aircraft were pioneered by Bloy et al [1][2][3][4][5], and the results obtained were in good agreement with the wind tunnel experimental data. Venkataramanan and Dogan [7] developed the Vortex Effect Modeling Technique (VEMT) to simulate the flow field of aerial refueling.…”
Section: Introductionsupporting
confidence: 58%
“…In 1975, Jewell and Stapleford [10] and Rossow et al [18] proposed a mathematical model to describe the effect of wake. Modeling and analysis of the effect of a tanker's wake on a receiver aircraft were pioneered by Bloy et al [1][2][3][4][5], and the results obtained were in good agreement with the wind tunnel experimental data. Venkataramanan and Dogan [7] developed the Vortex Effect Modeling Technique (VEMT) to simulate the flow field of aerial refueling.…”
Section: Introductionsupporting
confidence: 58%
“…Unsteady wing-wake interaction research has undergone profound growth in recent years as researchers utilize knowledge of wake impingement to develop new multi-vehicle flight formations, design novel micro-air vehicles [26], and leverage inspirations from biological swimmers and flyers [13]. Examples of such interactions include close formation flight [2], wake-induced flutter [5,23,12], aerial refueling [3], and fish schooling dynamics [21]. Although diverse in applications, the fundamental thread through this area of research is the characterization of interactions between unsteady wakes and lifting bodies.…”
Section: Introductionmentioning
confidence: 99%
“…It is believed that aircraft formation control will play a fundamental role in future aerospace scenarios, where unmanned air vehicles will be required to manoeuvre in swarms for surveillance, reconnaissance and rescue purposes in hostile environments (2) . Finally, autonomous formation flight systems are widely investigated due to their close connection to the aerial refuelling problem (3,4) . Most of the existing literature concerning the problem of aircraft formation control (5)(6)(7)(8)(9) and/or aerodynamic interference modelling (10)(11)(12) , assumes a fixed formation structure.…”
Section: Introductionmentioning
confidence: 99%