2018
DOI: 10.1016/j.heliyon.2018.e01019
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Optimization of positional parameters of close-formation flight for blended-wing-body configuration

Abstract: In the present study, we study formation flight with two flying wing configurations. A low speed wind tunnel test is conducted to validate the accuracy of the Computational Fluid Dynamics (CFD). Two optimization procedures are implemented at a high subsonic speed. The free stream Mach number is kept at 0.85, the lead aircraft's angle of attack is 2°, and the following aircraft's angle of attack is 2° as well. The maximum lift-to-drag ratio of the following aircraft is achieved as the lateral spacing is 0.853 b… Show more

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Cited by 7 publications
(2 citation statements)
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“…An example of RBF meta-modeling in aerospace is the prediction of aerodynamic coefficients for a blended-wing-body (BWB) configuration. In a recent study, researchers used RBF to build a surrogate model for the prediction of lift and drag coefficients for a BWB configuration [31]. Another example is the use of RBF for the optimization of winglet spanwise camber morphing at different flight phases [32].…”
Section: Multivariate Adaptive Regression Splines (Mars) -It Is a Reg...mentioning
confidence: 99%
“…An example of RBF meta-modeling in aerospace is the prediction of aerodynamic coefficients for a blended-wing-body (BWB) configuration. In a recent study, researchers used RBF to build a surrogate model for the prediction of lift and drag coefficients for a BWB configuration [31]. Another example is the use of RBF for the optimization of winglet spanwise camber morphing at different flight phases [32].…”
Section: Multivariate Adaptive Regression Splines (Mars) -It Is a Reg...mentioning
confidence: 99%
“…The calculation adopts the in house calculation program, and has carried out a number of research work. [7][8][9] 2.2. Turbulence model Spalart-Allmaras(SA) turbulence model [10] is used for calculation.…”
Section: Introductionmentioning
confidence: 99%