Numerical and experimental study of the tolerance of natural laminar flow on a wing to TS destabilisation at the leading edge /wing-box junction

R. Ashworth; S. Lawson; R. Lowry; A. Martinez-Cava; S. Mughal; H. Roland; C. Thomas

Numerical and experimental study of the tolerance of natural laminar flow on a wing to TS destabilisation at the leading edge /wing-box junction

R. Ashworth, S. Lawson, R. Lowry, A. Martinez-Cava, S. Mughal, H. Roland, C. Thomas

Research output: Chapter in Book/Report/Conference proceeding › Conference proceeding contribution

Original language	English
Title of host publication	2016 Applied Aerodynamics Conference
Subtitle of host publication	evolution and innovation continues : the next 150 years of concepts, design and operations : conference programme and proceedings : 19-21, July 2016, Bristol
Publisher	Royal Aeronautical Society
Pages	336-349
Number of pages	14
ISBN (Electronic)	9781857683714
Publication status	Published - 2016
Externally published	Yes

Cite this

Ashworth, R., Lawson, S., Lowry, R., Martinez-Cava, A., Mughal, S., Roland, H., & Thomas, C. (2016). Numerical and experimental study of the tolerance of natural laminar flow on a wing to TS destabilisation at the leading edge /wing-box junction. In 2016 Applied Aerodynamics Conference: evolution and innovation continues : the next 150 years of concepts, design and operations : conference programme and proceedings : 19-21, July 2016, Bristol (pp. 336-349). Royal Aeronautical Society.

Ashworth, R. ; Lawson, S. ; Lowry, R. ; Martinez-Cava, A. ; Mughal, S. ; Roland, H. ; Thomas, C. / Numerical and experimental study of the tolerance of natural laminar flow on a wing to TS destabilisation at the leading edge /wing-box junction. 2016 Applied Aerodynamics Conference: evolution and innovation continues : the next 150 years of concepts, design and operations : conference programme and proceedings : 19-21, July 2016, Bristol. Royal Aeronautical Society, 2016. pp. 336-349

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title = "Numerical and experimental study of the tolerance of natural laminar flow on a wing to TS destabilisation at the leading edge /wing-box junction",

author = "R. Ashworth and S. Lawson and R. Lowry and A. Martinez-Cava and S. Mughal and H. Roland and C. Thomas",

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Ashworth, R, Lawson, S, Lowry, R, Martinez-Cava, A, Mughal, S, Roland, H & Thomas, C 2016, Numerical and experimental study of the tolerance of natural laminar flow on a wing to TS destabilisation at the leading edge /wing-box junction. in 2016 Applied Aerodynamics Conference: evolution and innovation continues : the next 150 years of concepts, design and operations : conference programme and proceedings : 19-21, July 2016, Bristol. Royal Aeronautical Society, pp. 336-349.

Numerical and experimental study of the tolerance of natural laminar flow on a wing to TS destabilisation at the leading edge /wing-box junction. / Ashworth, R.; Lawson, S.; Lowry, R.; Martinez-Cava, A.; Mughal, S.; Roland, H.; Thomas, C.

2016 Applied Aerodynamics Conference: evolution and innovation continues : the next 150 years of concepts, design and operations : conference programme and proceedings : 19-21, July 2016, Bristol. Royal Aeronautical Society, 2016. p. 336-349.

Research output: Chapter in Book/Report/Conference proceeding › Conference proceeding contribution

TY - GEN

T1 - Numerical and experimental study of the tolerance of natural laminar flow on a wing to TS destabilisation at the leading edge /wing-box junction

AU - Ashworth, R.

AU - Lawson, S.

AU - Lowry, R.

AU - Martinez-Cava, A.

AU - Mughal, S.

AU - Roland, H.

AU - Thomas, C.

PY - 2016

Y1 - 2016

M3 - Conference proceeding contribution

SP - 336

EP - 349

BT - 2016 Applied Aerodynamics Conference

PB - Royal Aeronautical Society

ER -

Ashworth R, Lawson S, Lowry R, Martinez-Cava A, Mughal S, Roland H et al. Numerical and experimental study of the tolerance of natural laminar flow on a wing to TS destabilisation at the leading edge /wing-box junction. In 2016 Applied Aerodynamics Conference: evolution and innovation continues : the next 150 years of concepts, design and operations : conference programme and proceedings : 19-21, July 2016, Bristol. Royal Aeronautical Society. 2016. p. 336-349