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Aerospace, Volume 2, Issue 2

2015 June - 11 articles

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Articles (11)

  • Article
  • Open Access
15 Citations
11,699 Views
23 Pages

Shock Wave Attenuation Using Foam Obstacles: Does Geometry Matter?

  • Hongjoo Jeon,
  • Jonathan R. Gross,
  • Sarah Estabrook,
  • Stylianos Koumlis,
  • Qian Wan,
  • Gauri R. Khanolkar,
  • Xingtian Tao,
  • David M. Mensching,
  • Edward J. Lesnick and
  • Veronica Eliasson

15 June 2015

A shock wave impact study on open and closed cell foam obstacles was completed to assess attenuation effects with respect to different front face geometries of the foam obstacles. Five different types of geometries were investigated, while keeping th...

  • Article
  • Open Access
17 Citations
9,978 Views
28 Pages

5 June 2015

Multirotor is the umbrella term for the family of unmanned aircraft, which include the quadrotor, hexarotor and other vertical take-off and landing (VTOL) aircraft that employ multiple main rotors for lift and control. Development and testing of nove...

  • Communication
  • Open Access
1 Citations
7,861 Views
13 Pages

4 June 2015

An Unmanned Aerial System (UAS) has been developed which is based on an aerodynamically functionalized planar wideband antenna. The antenna utilizes a planar circular dipole metallization scheme. The aerodynamic structure implements a planform simila...

  • Article
  • Open Access
8 Citations
8,721 Views
33 Pages

28 May 2015

This numerical study focuses on the fire phenomenology associated with the presence of a composite-type aircraft immersed, at one particular location and orientation, within a large aviation-fuel fire in a moving fluid medium. An extension of the edd...

  • Article
  • Open Access
33 Citations
39,686 Views
44 Pages

13 May 2015

In this paper, an ornithopter prototype that mimics the flapping motion of bird flight is developed, and the lift and thrust generation characteristics of different wing designs are evaluated. This project focused on the spar arrangement and material...

  • Article
  • Open Access
2 Citations
9,133 Views
13 Pages

4 May 2015

Unmanned aircraft must be characterized by a level of safety, similar to that of manned aircraft, when performing flights over densely populated areas. Dangerous situations or emergencies are frequently connected with the necessity to change the prof...

  • Review
  • Open Access
13 Citations
9,735 Views
19 Pages

30 April 2015

Research on shock wave mitigation in channels has been a topic of much attention in the shock wave community. One approach to attenuate an incident shock wave is to use obstacles of various geometries arranged in different patterns. This work is insp...

  • Article
  • Open Access
15 Citations
9,945 Views
18 Pages

Development of Flight Path Planning for Multirotor Aerial Vehicles

  • Yi-Ju Tsai,
  • Chia-Sung Lee,
  • Chun-Liang Lin and
  • Ching-Huei Huang

27 April 2015

This study addresses the flight-path planning problem for multirotor aerial vehicles (AVs). We consider the specific features and requirements of real-time flight-path planning and develop a rapidly-exploring random tree (RRT) algorithm to determine...

  • Review
  • Open Access
24 Citations
11,022 Views
14 Pages

27 April 2015

The aerospace community is planning for growth in Unmanned Aerial Systems (UAS) funding and research opportunities. The premise that UAS will revolutionize aerospace appears to be unfolding based on current trends. There is also an anticipation of an...

  • Article
  • Open Access
6 Citations
7,680 Views
16 Pages

21 April 2015

This paper presents a semi-analytical trajectory planning method for quadrotor UAVs. These trajectories are analytically defined, are constant in speed and sub-optimal with respect to a weighted quadratic cost function of the translational and angula...

  • Article
  • Open Access
44 Citations
13,182 Views
20 Pages

Gust Alleviation of a Large Aircraft with a Passive Twist Wingtip

  • Shijun Guo,
  • Jaime Espinosa De Los Monteros and
  • Ying Liu

3 April 2015

This paper presents an investigation into the gust response and wing structure load alleviation of a 200-seater aircraft by employing a passive twist wingtip (PTWT). The research was divided into three stages. The first stage was the design and anal...

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Aerospace - ISSN 2226-4310