Aerodynamic prediction of a projectile fitted with fins. Issue 5 (8th May 2018)

• Record Type: Journal Article
• Authors: Decrocq, Cédric; Martinez, Bastien; Albisser, Marie; Dobre, Simona; Gnemmi, Patrick; Bailly, Yannick; Roy, Jean-Claude
• Is Part Of: International journal of numerical methods for heat & fluid flow. Volume 28:Issue 5(2018)
• Page Start: 1218
• Page End: 1236
• Publication Date: 2018-05-08
• Subjects: Aerodynamics -- Computational fluid dynamics -- Aeroballistics -- Free-flight experiments -- Semi-empirical predictions -- Wind-tunnel experiments; Heat -- Transmission -- Mathematics -- Periodicals; Fluid dynamics -- Mathematics -- Periodicals; 536.2
• DOI: 10.1108/HFF-06-2017-0259
• Languages: English
• ISSNs: 0961-5539

Abstract

Abstract : Purpose: The present paper deals with weapon aerodynamics and aims to describe preliminary studies that were conducted for developing the next generation of long-range guided ammunition. Over history, ballistic research scientists were constantly investigating new artillery systems capable of overcoming limitations of range, accuracy and manoeuvrability. While futuristic technologies are increasingly under development, numerous issues concerning current powdered systems still need to be addressed. In this context, the present work deals with the design and the optimization of a new concept of long-range projectile with regard to multidisciplinary fields, including flight scenario, steering strategy, mechanical actuators or size of payload. Design/methodology/approach: Investigations are conducted for configurations that combine existing full calibre 155 mm guided artillery shell with a set of lifting surfaces. As the capability of the ammunition highly depends on lifting surfaces in terms of number, shape or position, a parametric study has to be conducted for determining the best aerodynamic architecture. To speed-up this process, initial estimations are conducted thanks to low computational cost methods suitable for preliminary design requirements, in terms of time, accuracy and flexibility. The WASP code (Wing-Aerodynamic-eStimation-for-Projectiles) has been developed for rapidly predicting aerodynamic coefficients (static and dynamic) of a set of lifting surfaces fitted on a projectile fuselage, as a function of geometry and flight conditions, up to transonic velocities. Findings: In the present study, WASP predictions at Mach 0.7 of both normal force and pitching moment coefficients are assessed for two configurations. Originality/value: Analysis is conducted by gathering results from WASP, computational-fluid-dynamics (CFD) simulations, wind-tunnel experiments and free-flight tests. Obtained results demonstrate the ability of WASP code to be used for preliminary design steps.