Print Email Facebook Twitter Flow analysis of hammerhead launcher geometries in the transonic regime Title Flow analysis of hammerhead launcher geometries in the transonic regime Author D'Aguanno, A. (TU Delft Aerodynamics) González Romero, A. (Student TU Delft) Schrijer, F.F.J. (TU Delft Aerodynamics) van Oudheusden, B.W. (TU Delft Aerodynamics) Date 2024 Abstract Hammerhead launcher configurations, characterized by a larger diameter in the payload fairing than the rest of the launch vehicle, face substantial challenges during transonic operations due to their susceptibility to flow separation and intense pressure fluctuations. This experimental study investigates the influence of the nose and boat-tail geometry on the flow around hammerhead configurations in the transonic regime (Ma=0.7-0.8) and for various angles of attack (α=0-4°). To gain a general understanding of the main flow features, such as shockwave formation, separated flow in the boat tail region, and flow reattachment, oil flow and schlieren visualizations were employed. Schlieren visualizations were also utilized to characterize the level of unsteadiness in these regions. Additionally, particle image velocimetry (PIV) was employed to quantify variations in the velocity field. The study's findings reveal an optimization of flow performance in the presence of a bi-conic nose, attributed to the creation of two-shockwave structures with relatively low intensity. This is in contrast to the ogive and conic noses, which exhibit a single, more detrimental shockwave structure (with the conic nose being the least favorable configuration). The investigation into different boat tail angles indicates that adopting low-angle boat tails (5° and 15° compared to 34°) leads to a noticeable reduction in the separated area, albeit associated with an increase in the range of oscillation of the shockwave structures. To reference this document use: http://resolver.tudelft.nl/uuid:057a5556-2e58-44c5-acc9-5b78b96a0140 DOI https://doi.org/10.2514/6.2024-2145 Publisher American Institute of Aeronautics and Astronautics Inc. (AIAA) ISBN 978-1-62410-711-5 Source Proceedings of the AIAA SCITECH 2024 Forum Event AIAA SCITECH 2024 Forum, 2024-01-08 → 2024-01-12, Orlando, United States Part of collection Institutional Repository Document type conference paper Rights © 2024 A. D'Aguanno, A. González Romero, F.F.J. Schrijer, B.W. van Oudheusden Files PDF d_aguanno_et_al_2024_flow ... regime.pdf 1.65 MB Close viewer /islandora/object/uuid:057a5556-2e58-44c5-acc9-5b78b96a0140/datastream/OBJ/view