Aerodynamic interactions of a Reusable Launch Vehicle model with different nose configurations
Sign Up to like & getrecommendations! Published in 2020 at "Acta Astronautica"
DOI: 10.1016/j.actaastro.2020.07.022
Abstract: Abstract The Two-Stage-To-Orbit (TSTO) hypersonic vehicle is an example of a Reusable Launch Vehicle (RLVs) configuration, and it has the advantages of small mass and large payload. A TSTO concept aircraft comprising a booster and… read more here.
Keywords: nose configurations; vehicle; reusable launch; launch vehicle ... See more keywords
Experimental study on quasi-static penetration process of cylindrical indenters with different nose shapes into the hybrid composite panels
Sign Up to like & getrecommendations! Published in 2019 at "Journal of Composite Materials"
DOI: 10.1177/0021998318780490
Abstract: The main aim of the present research is to investigate the quasi-static penetration process of cylindrical indenters with different nose shapes into multilayered composite panels made of Dyneema and Glass woven fibers, and aluminum face… read more here.
Keywords: quasi static; nose shapes; composite panels; static penetration ... See more keywords
Hypersonic Aeroheating Characteristics of Leading Edges with Different Nose Radii
Sign Up to like & getrecommendations! Published in 2017 at "Journal of Thermophysics and Heat Transfer"
DOI: 10.2514/1.t4950
Abstract: The applications of leading edges with different nose radii in hypersonic flights require investigations on their aeroheating characteristics in various gas flow regimes. For a detailed numerical s... read more here.
Keywords: leading edges; nose radii; different nose; edges different ... See more keywords