A Summary of the Forebody High-Angle-of-Attack Aerodynamics Research on the F-18 and the X-29A Aircraft 921996
High-angle-of-attack aerodynamic studies have been conducted on both the F-18 High Alpha Research Vehicle (HARV) and the X-29A aircraft. Data obtained include on- and off-surface flow visualization and static pressure measurements on the forebody. Comparisons of similar results are made between the two aircraft where possible. The forebody shapes of the two aircraft are different and the X-29A forebody flow is affected by the addition of nose strakes and a flight test noseboom. The forebody flow field of the F-18 HARV is fairly symmetric at zero sideslip and has distinct, well-defined vortices. The X-29A forebody vortices are more diffuse and are sometimes asymmetric at zero sideslip. These asymmetries correlate with observed zero-sideslip aircraft yawing moments.
Citation: Bjarke, L., Del Frate, J., and Fisher, D., "A Summary of the Forebody High-Angle-of-Attack Aerodynamics Research on the F-18 and the X-29A Aircraft," SAE Technical Paper 921996, 1992, https://doi.org/10.4271/921996. Download Citation
Lisa J. Bjarke, John H. Del Frate, David F. Fisher
NASA Dryden Flight Research Facility
Aerospace Technology Conference and Exposition
SAE 1992 Transactions: Journal of Aerospace-V101-1