Effect of modifications to island shape and geometrical configuration on the external aerodynamics of a generic aircraft carrier

被引:1
作者
Mathew, Marthamootil Philipose [1 ,3 ]
Singh, Sidh Nath [1 ]
Sinha, Sawan Suman [1 ]
Vijayakumar, Rajgopalan [2 ]
机构
[1] Indian Inst Technol, Dept Appl Mech, Delhi, India
[2] Indian Inst Technol, Dept Ocean Engn, Chennai, India
[3] Indian Inst Technol Delhi, Dept Appl Mech, Appl Mech, Room 354, New Delhi 110016, India
关键词
computational fluid dynamics; external aerodynamics; aircraft carrier; airwake studies; PASSIVE FLOW-CONTROL; SKI-JUMP;
D O I
10.1177/09544100221138919
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The external aerodynamics of an aircraft carrier plays a vital role in the safe landing of aircraft during take-off and recovery. The hull, flight deck, and the island create a turbulent disturbance behind the aircraft carrier, leading to a simultaneous reduction in forward velocity and a downwash, which together create a sinking effect on the aircraft along its glideslope path. This phenomenon is known as the burble effect. It could potentially increase the pilot's workload and strain their mental and physical faculties. Any design change that obviates or reduces the burble effect would potentially increase the probability of safely landing the aircraft on an aircraft carrier. There are only a few studies on the external aerodynamics of an aircraft carrier. The primary motivation of this study is to evaluate the effect of modifications to the island structure on the external aerodynamics of a generic aircraft carrier, especially the burble behind the carrier. The first part of the study pertains to the parametric changes to the aspect ratio of the island, that is, its length to width ratio and the consequent impact on the aerodynamics behind the carrier along the flight glide path. The second part of the study focuses on changing the geometry of the island by rounding the assumed cuboid island's sharp corners, and evaluating its effect on the burble along the glideslope path of the aircraft. For the study, computational fluid dynamics (CFD) analysis on a generic aircraft carrier model has been carried out using the commercially available CFD solver Ansys FLUENT. The CFD studies have been validated by results of experiments conducted in a wind tunnel on the same generic aircraft carrier model. From the studies, it is seen that the aspect ratio of the island greater than one and rounding the sharp edges of the island have beneficial effects in reducing the impact of the burble behind the carrier.
引用
收藏
页码:1835 / 1854
页数:20
相关论文
共 30 条
  • [21] Polsky S., AIAA MODELING SIMULA, DOI DOI 10.2514/6.2005-6298
  • [22] Polsky S., 2002, Proc. 40th AIAA Aerosp. Sci. Meeting Exhib, P1, DOI DOI 10.2514/6.2002-1022
  • [23] Ringleb FO., 1963, NAELENG7019
  • [24] RUDOWSKY T., 2002, REV CARRIER APPROACH
  • [25] Shipman J., 2005, 43 AIAA AER SCI M EX, P1, DOI [10.2514/6.2005-1105, DOI 10.2514/6.2005-1105]
  • [26] Smith DouglasV., 2010, One Hundred Years of U.S. Navy Air Power
  • [27] Pressure and velocity measurements of air flow past a proposed generic Aircraft carrier geometry
    Vignesh Kumar, Kishore
    Nasiruddin, Sheikh
    Shukla, Shrish
    Singh, Sidh Nath
    Sinha, Sawan Suman
    Vijayakumar, Rajgopalan
    [J]. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART M-JOURNAL OF ENGINEERING FOR THE MARITIME ENVIRONMENT, 2022, 236 (02) : 326 - 345
  • [28] FLIGHT DECK DESIGN GUIDELINES
    VITALE, DJ
    [J]. NAVAL ENGINEERS JOURNAL, 1978, 90 (02) : 137 - 148
  • [29] Vivaldi B.E., 2004, Masters Thesis
  • [30] Computational and experimental modelling study of the unsteady airflow over the aircraft carrier HMS Queen Elizabeth
    Watson, N. A.
    Kelly, M. F.
    Owen, I.
    Hodge, S. J.
    White, M. D.
    [J]. OCEAN ENGINEERING, 2019, 172 : 562 - 574