Most cited
This page lists all time most cited articles for this title. Please use the publication date filters on the left if you would like to restrict this list to recently published content, for example to articles published in the last three years. The number of times each article was cited is displayed to the right of its title and can be clicked to access a list of all titles this article has been cited by.
- Cited by 5
Effect of counterflow argon plasma jet on aerodynamic drag of a blunt body at hypersonic Mach numbers
-
- Published online by Cambridge University Press:
- 16 June 2022, pp. 683-687
-
- Article
- Export citation
- Cited by 5
Relative rotor phasing for multicopter vibratory load minimisation
- Part of:
-
- Published online by Cambridge University Press:
- 21 October 2021, pp. 710-729
-
- Article
- Export citation
- Cited by 5
Non-linear aeroelastic response of high aspect-ratio wings in the frequency domain
-
- Published online by Cambridge University Press:
- 11 May 2017, pp. 858-876
-
- Article
- Export citation
- Cited by 5
On the chordwise lift distribution at the centre of swept wings
-
- Published online by Cambridge University Press:
- 07 June 2016, pp. 146-154
-
- Article
- Export citation
- Cited by 5
The numerical simulation of flow about installed aero engine nacelle using a finite element Euler solver on unstructured meshes
-
- Published online by Cambridge University Press:
- 04 July 2016, pp. 224-232
-
- Article
- Export citation
- Cited by 5
Highlights of the Lockheed Martin F-35 STOVL jet effects programme
-
- Published online by Cambridge University Press:
- 03 February 2016, pp. 119-127
-
- Article
- Export citation
- Cited by 5
Kinematic characteristics of longitudinal double folding wings
-
- Published online by Cambridge University Press:
- 17 June 2021, pp. 1977-2001
-
- Article
- Export citation
- Cited by 5
The dynamic induced velocity field of a model rotor in hover conditions
-
- Published online by Cambridge University Press:
- 04 July 2016, pp. 331-336
-
- Article
- Export citation
- Cited by 5
Plasto-Elastic Stress Distributions in Lugs
-
- Published online by Cambridge University Press:
- 07 June 2016, pp. 230-246
-
- Article
- Export citation
- Cited by 5
Hybrid high-order sliding mode-based control for multivariable cross-coupling systems: Scale-laboratory helicopter system application
-
- Published online by Cambridge University Press:
- 27 June 2017, pp. 1319-1341
-
- Article
- Export citation
- Cited by 5
Measurements of velocities in the near field of a lobed forced mixer trailing edge
-
- Published online by Cambridge University Press:
- 04 July 2016, pp. 121-129
-
- Article
- Export citation
- Cited by 5
The Sound of Rotorcraft
-
- Published online by Cambridge University Press:
- 04 July 2016, pp. 385-397
-
- Article
- Export citation
- Cited by 5
Static and dynamic pitch stability of a blunted cone with forward facing aerodynamic spike in hypersonic flow
-
- Published online by Cambridge University Press:
- 04 July 2016, pp. 307-314
-
- Article
- Export citation
- Cited by 5
The Static Aeroelastic Deformation of Slender Configurations*: Part II: Some Calculations on Slender Plate Aircraft, Including Non-Linear Aerodynamics
-
- Published online by Cambridge University Press:
- 07 June 2016, pp. 372-394
-
- Article
- Export citation
- Cited by 5
Re-entry guidance method based on decoupling control variables and waypoint
-
- Published online by Cambridge University Press:
- 05 April 2019, pp. 523-535
-
- Article
- Export citation
- Cited by 5
Diagonally dominant backstepping autopilot for aircraft with unknown actuator failures and severe winds
-
- Published online by Cambridge University Press:
- 27 January 2016, pp. 1009-1038
-
- Article
- Export citation
- Cited by 5
Two-Dimensional Bow Shock Wave Detachment Distances
-
- Published online by Cambridge University Press:
- 28 July 2016, pp. 424-426
-
- Article
- Export citation
- Cited by 5
Acoustic validation of a new code using particle wake aerodynamics and geometrically-exact beam structural dynamics
-
- Published online by Cambridge University Press:
- 03 February 2016, pp. 257-267
-
- Article
- Export citation
- Cited by 5
Downward pointing winglet design and assessment within the M-DAW research project
-
- Published online by Cambridge University Press:
- 03 February 2016, pp. 221-232
-
- Article
- Export citation
- Cited by 5
Turboprop aircraft noise: Advancements and comparison with flyover data
- Part of:
-
- Published online by Cambridge University Press:
- 27 January 2016, pp. 565-589
-
- Article
- Export citation