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A new method to reduce the noise of the miniaturised inertial sensors disposed in redundant linear configurationsGRIGORIE, T. L; BOTEZ, R. M.Aeronautical Journal. 2013, Vol 117, Num 1188, pp 111-132, issn 0001-9240, 22 p.Article

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Aerodynamics and aerodynamic research in Formula 1TOET, W.Aeronautical Journal. 2013, Vol 117, Num 1187, pp 1-26, issn 0001-9240, 26 p.Article

Progressive failure analysis for the interaction of interlaminar and intralaminar failure modes in composite structures with an initial delaminationJI, W; WAAS, A. M.Aeronautical Journal. 2013, Vol 117, Num 1187, pp 71-85, issn 0001-9240, 15 p.Article

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Simulations of a low-boom, axisymmetric, external compression inletCOYNE, T; LOTH, E; KONCSEK, J et al.Aeronautical Journal. 2013, Vol 117, Num 1193, pp 709-726, issn 0001-9240, 18 p.Article

The influence of simulated missile warhead fragment damage on the aerodynamic characteristics of two-dimensional wingsIRWIN, A. J; RENDER, P. M.Aeronautical Journal. 2013, Vol 117, Num 1194, pp 823-837, issn 0001-9240, 15 p.Article

The influence of transition onset location on the performance of shock control bumpsMCINTOSH, S. C; QIN, N.Aeronautical Journal. 2013, Vol 117, Num 1196, pp 1037-1051, issn 0001-9240, 15 p.Article

Validation of endurance estimates for battery powered UAVsTRAUB, L. W.Aeronautical Journal. 2013, Vol 117, Num 1197, pp 1155-1166, issn 0001-9240, 12 p.Article

Vision guidance of a fixed wing UAV using a single camera configurationLONG, P.-T; CHEN, S.-H; YANG, Y et al.Aeronautical Journal. 2013, Vol 117, Num 1188, pp 147-173, issn 0001-9240, 27 p.Article

Wing mass estimation algorithm for medium range box wing aircraftJEMITOLA, P. O; MONTERZINO, G; FIELDING, J et al.Aeronautical Journal. 2013, Vol 117, Num 1189, pp 329-340, issn 0001-9240, 12 p.Article

Spin induced aerodynamic flow conditions on full-scale aeroplane wing and horizontal tail surfacesHOFF, R. I; GRATTON, G. B.Aeronautical Journal. 2013, Vol 117, Num 1198, pp 1207-1231, issn 0001-9240, 25 p.Article

Stalling transport aircraftBOLDS-MOOREHEAD, P. J; CHANEY, V. G; LUTZ, T et al.Aeronautical Journal. 2013, Vol 117, Num 1198, pp 1183-1206, issn 0001-9240, 24 p.Article

A career in vortices and edge forcesLAMAR, J.Aeronautical Journal. 2012, Vol 116, Num 1176, pp 101-152, issn 0001-9240, 52 p.Article

Aircraft conceptual design for optimal environmental performanceHENDERSON, R. P; MARTINS, J. R. R. A; PEREZ, R. E et al.Aeronautical Journal. 2012, Vol 116, Num 1175, pp 1-22, issn 0001-9240, 22 p.Article

Camera tracking and qualitative airflow assessment of a two-turn erect spinHOFF, R. I; GRATTON, G. B.Aeronautical Journal. 2012, Vol 116, Num 1179, pp 541-562, issn 0001-9240, 22 p.Article

Effects of targeting pod modification on F/A-18C Hornet weapons releaseO'BRIEN, C. W; SNYDER, M. R; HALLBERG, E. N et al.Aeronautical Journal. 2012, Vol 116, Num 1181, pp 743-755, issn 0001-9240, 13 p.Article

Hovering rotor computations using an aeroelastic blade modelDEHAEZE, F; BARAKOS, G. N.Aeronautical Journal. 2012, Vol 116, Num 1180, pp 621-649, issn 0001-9240, 29 p.Article

In-flight Ice formation simulation on finite wings and air intakesOZGEN, S; CAMBEK, M.Aeronautical Journal. 2012, Vol 116, Num 1178, pp 337-362, issn 0001-9240, 26 p.Article

On the generation of the mean velocity profile for turbulent boundary layers with pressure gradient under equilibrium conditionsRONA, A; MONTI, M; AIRIAU, C et al.Aeronautical Journal. 2012, Vol 116, Num 1180, pp 569-598, issn 0001-9240, 30 p.Article

Operational performance of inlet barrier filters for rotorcraftBOJDO, N; FILIPPONE, A.Aeronautical Journal. 2012, Vol 116, Num 1182, pp 847-869, issn 0001-9240, 23 p.Article

Performance of Glare panels subjected to intense pressure pulse loadingSOUTIS, C; MOHAMED, G; HODZIC, A et al.Aeronautical Journal. 2012, Vol 116, Num 1180, pp 667-679, issn 0001-9240, 13 p.Article

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Use of aerofoil section dynamic stall synthesis methods in rotor designCHAN, W; PERRY, J.Aeronautical Journal. 2012, Vol 116, Num 1179, pp 501-520, issn 0001-9240, 20 p.Article