Hybrid Grid Solutions on the (CAWAPI) F-16XL Using Falcon v4

USM3D Unstructured Grid Solutions for CAWAPI at NASA LaRC

“…In general, the USM3D predictions agree better with measured data than those from CFL3D:BL-DS 4 , but both solutions only fairly approximate the measurements. Similar trends are noted by others in the CAWAPI facet [7][8][9][10][11][12][13][14][15] of the AVT-113 task group. Moreover, from Fig.…”

PAB3D Simulations for the CAWAPI F-16XL

“…For this purpose, new and existing CFD codes have to be validated, and their Technology Readiness Level checked and/or increased. To meet these objectives, several numerical studies [7][8][9][10][11][12][13][14][15][16] have been conducted to compute and compare predicted flow around the F-16XL with flight data. CAWAPI members embraced the idea of engaging in a cooperative venture.…”

A Survey of Factors Affecting Blunt-Leading-Edge Separation for Swept and Semi-Slender Wings

“…CFD solutions were contributed from nine groups using ten different solvers, including both structured and unstructured approaches, to assess predictive capabilities for these data. Two special sessions at the 45 th AIAA Aerospace Sciences meeting highlighted these individual contributions [references [47][48][49][50][51][52][53][54][55][56][57], and a summary paper by Rizzi 57 [2007] was also included. Considerable effort went toward modeling the complex aircraft geometry at the high Reynolds numbers of the flight test data.…”