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Aerospace, Volume 5, Issue 3

September 2018 - 32 articles

Cover Story: As a result of pursuing high efficiency, Cooling technology has become critical in modern gas turbine design. To protect the most vulnerable part of the turbine from thermal damage, various cooling schemes has been tested in the blade tip region in the past few decades. The present article summarizes the most recent progresses in this area, which were reported by researchers all around the world, provides a good insight of the tip cooling characteristics, and exhibits the frontier of research directions for the future. View this paper.
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Articles (32)

  • Article
  • Open Access
7 Citations
15,118 Views
32 Pages

The calculation of rocket trajectories is most often performed using purely numerical methods that account for all relevant parameters and provide the required results. There is a complementary need for analytical methods that make more explicit the...

  • Review
  • Open Access
83 Citations
16,100 Views
24 Pages

Although structural health monitoring (SHM) technologies using sensors have dramatically been developed recently, their capability should be evaluated from the perspective of the maintenance industry. As a first step toward utilizing sensors, the obj...

  • Article
  • Open Access
14 Citations
7,078 Views
19 Pages

Adaptive Feedforward Control for Gust-Induced Aeroelastic Vibrations

  • Yongzhi Wang,
  • Andrea Da Ronch and
  • Maryam Ghandchi Tehrani

This paper demonstrates the implementation of an adaptive feedforward controller to reduce structural vibrations on a wing typical section. The aeroelastic model includes a structural nonlinearity, which is modelled in a polynomial form. Aeroelastic...

  • Article
  • Open Access
14 Citations
7,106 Views
19 Pages

Simulation and Experimental Evaluation of a Flexible Time Triggered Ethernet Architecture Applied in Satellite Nano/Micro Launchers

  • Vincenzo Eramo,
  • Francesco G. Lavacca,
  • Francesco Valente,
  • Andrea Pisculli and
  • Stefano Caporossi

The success of small satellites has lead to the study of new technologies for the realization of Nano and Micro Launch Vehicle (NMLV) in order to make competitive launch costs. The paper has the objective to define and experimentally investigate the...

  • Article
  • Open Access
23 Citations
8,195 Views
26 Pages

A careful arrival and departure sequencing of aircraft can reduce the inter-arrival/departure time, thereby opening up opportunities for new landing and/or take-off slots, which may increase the runway throughput. This sequence when serviced with a s...

  • Article
  • Open Access
14 Citations
7,991 Views
12 Pages

Beetles have attracted attention from researchers due to their unique combination of a passively flapping forewing and an actively flapping hindwing during flight. Because the wing loads of beetles are larger than the wing loads of other insects, the...

  • Article
  • Open Access
17 Citations
7,671 Views
16 Pages

Labyrinth seals are a state-of-the-art sealing technology to prevent and control leakage flows at rotor–stator interfaces in turbomachinery. Higher pressure ratios and the economical use of cooling air require small clearances, which lead to po...

  • Article
  • Open Access
22 Citations
9,529 Views
11 Pages

Life Cycle Assessment of Ramie Fiber Used for FRPs

  • Shaoce Dong,
  • Guijun Xian and
  • Xiao-Su Yi

With the depletion of natural resources and the deterioration of environment, natural fiber based biomaterials are attracting more and more attentions. Natural fibers are considered to be renewable, biodegradable, and ecofriendly, and have been appli...

  • Article
  • Open Access
34 Citations
7,513 Views
13 Pages

Robust Optimization of Airplane Passenger Seating Assignments

  • R. John Milne,
  • Mostafa Salari and
  • Lina Kattan

We present a method that reduces the time it takes to complete the passenger boarding of an airplane. In particular, we describe a two-stage mixed integer programming (MIP) approach, which assigns passengers to seats on an airplane based on the numbe...

  • Article
  • Open Access
53 Citations
29,155 Views
20 Pages

Computational Study of Propeller–Wing Aerodynamic Interaction

  • Pooneh Aref,
  • Mehdi Ghoreyshi,
  • Adam Jirasek,
  • Matthew J. Satchell and
  • Keith Bergeron

Kestrel simulation tools are used to investigate the mutual interference between the propeller and wing of C130J aircraft. Only the wing, nacelles, and propeller geometries are considered. The propulsion system modelled is a Dowty six-bladed R391 pro...

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Aerospace - ISSN 2226-4310