Effect of Tubercle Leading Edge Control Surface on the Performance of the Double Delta Wing Fighter Aircraft

Abstract

To improve the aerodynamic characteristics of the generic fighter aircraft by modifying the leading edge control surface of the tailless double delta wing. Simulations are carried out to determine the lift to drag ratio and pitching moment characteristics of the modified wing (Tubercle LEVCON) and compared with the existing fighter aircraft wing at low Mach numbers and high angles of attack, typically for landing/ takeoff configurations. The computational domain is meshed with unstructured grids and steady state Reynolds Averaged Navier Stokes (RANS) CFD simulations are carried out. Lift coefficient and drag coefficient are considered as the principle performance metrics for a control surface and pitching moment is determined for assessing the performance and longitudinal stability of the aircraft. Results obtained indicate that the tubercle wing increases the lift coefficient due to the vortex formation at each tubercle and the flow remains attached over the entire span of the wing.

Authors and Affiliations

P Sharmila, S Rajakumar

Keywords

Related Articles

Improve Cloud Data Storage Security Using Data Partition Technique

The rapid increment in the popularity of cloud storage services has lead the companies which handle the critical data for their storage needs using cloud services. Examples of critical data includes the dat abases of me...

A Low Power 4 Bit Successive Approximation Analog-To-Digital Converter Using 180nm Technology

In this paper, 4 bit successive approximation analog-to- digital converter (SAR ADC) has been designed. The design is using Cadence tool with 180nm CMOS technology in which supply voltage is 3.3V. The successive approxi...

Comparative Study of Various Binary Floating Point Multiplier Techniques Using VHDL

In computing, floating point describes a method of representing an approximation of a real number in a way that can support a wide range of values. Low power consumption and smaller area are some of the most important c...

slugUltra-wideband L-strip proximity coupled slot loaded semicircular microstrip antenna

An analysis and design of a nove l ultra wideband L - strip proximity coupled sl ot loaded semicircular micro strip antenna is proposed. The structure is simulated on MoM based IE3D si...

Time Series Analysis of Glacial Lake in Western Himalayas Based on NDWI and MNDWI

This Water always appears diversely, which makes its extraction not so simple. In this paper, we propose a new, simple, fast and accurate methodology based on a combination of the two indices NDWI and MNDWI for calculat...

Download PDF file
  • EP ID EP20949
  • DOI -
  • Views 253
  • Downloads 5

How To Cite

P Sharmila, S Rajakumar (2015). Effect of Tubercle Leading Edge Control Surface on the Performance of the Double Delta Wing Fighter Aircraft. International Journal for Research in Applied Science and Engineering Technology (IJRASET), 3(6), -. https://europub.co.uk/articles/-A-20949