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Aerospace, Volume 5, Issue 3

2018 September - 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
7,033 Views
16 Pages

19 September 2018

Components of aeronautical gas turbines are increasingly being constructed from two layers, including a pressure containing skin, which is then protected by a thermal tile. Between them, pedestals and/or other heat transfer enhancing features are oft...

(This article belongs to the Special Issue Secondary Air Systems in Gas Turbine Engines)
  • Article
  • Open Access
12 Citations
7,950 Views
23 Pages

Leading-Edge Roughness Affecting Diamond-Wing Aerodynamic Characteristics

  • Andrei Buzica,
  • Lisa Debschütz,
  • Florian Knoth and
  • Christian Breitsamter

19 September 2018

Diamond wing configurations for low signature vehicles have been studied in recent years. Yet, despite numerous research on highly swept, sharp edged wings, little research on aerodynamics of semi-slender wings with blunt leading-edges exists. This p...

(This article belongs to the Special Issue Feature Papers in Aerospace)
  • Article
  • Open Access
24 Citations
10,822 Views
17 Pages

10 September 2018

Free vibration (or eigenvalue analysis) is a prerequisite for aeroelastic analysis. For divergence analysis, slope influence coefficients (rotation at point i due to unit load at point j) are calculated using free vibration mode shapes and correspond...

(This article belongs to the Special Issue Aeroelasticity)
  • Article
  • Open Access
8 Citations
6,707 Views
10 Pages

Aerodynamic Design of a Laval Nozzle for Real Gas Using Hodograph Method

  • Aleksandr Chikitkin,
  • Mikhail Petrov,
  • Roman Dushkov and
  • Ernest Shifrin

10 September 2018

We propose an approach for the design of the subsonic part of plane and axisymmetric Laval nozzles for real gases. The proposed approach is based on the hodograph method and allows one to solve the inverse design problem directly. Real gas effects ar...

  • Article
  • Open Access
13 Citations
8,406 Views
21 Pages

Fast and Robust Flight Altitude Estimation of Multirotor UAVs in Dynamic Unstructured Environments Using 3D Point Cloud Sensors

  • Hriday Bavle,
  • Jose Luis Sanchez-Lopez,
  • Paloma De la Puente,
  • Alejandro Rodriguez-Ramos,
  • Carlos Sampedro and
  • Pascual Campoy

6 September 2018

This paper presents a fast and robust approach for estimating the flight altitude of multirotor Unmanned Aerial Vehicles (UAVs) using 3D point cloud sensors in cluttered, unstructured, and dynamic indoor environments. The objective is to present a fl...

(This article belongs to the Collection Unmanned Aerial Systems)
  • Article
  • Open Access
43 Citations
10,181 Views
12 Pages

2 September 2018

Ramie fabric-reinforced thermoset polylactic acid (PLA) composites were prepared by using heat pressing technology. Fabrics were treated with alkali, silane, and alkali–silane respectively, expecting an improvement of the interface between the fabric...

(This article belongs to the Special Issue ECO-COMPASS: Ecological and Multifunctional Composites for Application in Aircraft Interior and Secondary Structures)
  • Article
  • Open Access
15 Citations
17,894 Views
27 Pages

1 September 2018

The conceptual aircraft design and its integration with a combined cycle engine for hypersonic cruise at Mach 8 is documented in this paper. The paper describes the process taken to develop a hypersonic aircraft from a conceptual approach. The discus...

  • Article
  • Open Access
45 Citations
16,885 Views
24 Pages

1 September 2018

A method is presented to model the incompressible, attached, unsteady lift and pitching moment acting on a thin three-dimensional wing in the time domain. The model is based on the combination of Wagner theory and lifting line theory through the unst...

(This article belongs to the Special Issue Aeroelasticity)
  • Review
  • Open Access
26 Citations
17,825 Views
32 Pages

This article provides an overview of gas turbine blade tip external cooling technologies. It is not the intention to comprehensively review all the publications from past to present. Instead, selected reports, which represent the most recent progress...

  • Article
  • Open Access
7 Citations
7,909 Views
20 Pages

Changes in the amount and the distribution of mean and turbulent quantities in the free shear layer wake of a 2D National Advisory Committee for Aeronautics (NACA) 0012 airfoil and an AR 4 NACA 0012 wing with passive segmented rigid trailing edge (TE...

  • Article
  • Open Access
7 Citations
18,177 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...

(This article belongs to the Special Issue Feature Papers in Aerospace)
  • Review
  • Open Access
93 Citations
18,359 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...

(This article belongs to the Special Issue Civil and Military Airworthiness: Recent Developments and Challenges)
  • Article
  • Open Access
15 Citations
7,555 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...

(This article belongs to the Special Issue Aeroelasticity)
  • Article
  • Open Access
18 Citations
7,595 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...

(This article belongs to the Special Issue Verification Approaches for Nano- and Micro-Satellites)
  • Article
  • Open Access
25 Citations
8,872 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...

(This article belongs to the Collection Air Transportation—Operations and Management)
  • Article
  • Open Access
15 Citations
9,189 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...

(This article belongs to the Special Issue Bio-Inspired Aerospace System)
  • Article
  • Open Access
18 Citations
8,389 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...

(This article belongs to the Special Issue Secondary Air Systems in Gas Turbine Engines)
  • Article
  • Open Access
24 Citations
10,968 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...

(This article belongs to the Special Issue ECO-COMPASS: Ecological and Multifunctional Composites for Application in Aircraft Interior and Secondary Structures)
  • Article
  • Open Access
35 Citations
8,280 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...

(This article belongs to the Collection Air Transportation—Operations and Management)
  • Article
  • Open Access
64 Citations
32,352 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...

(This article belongs to the Special Issue Computational Aerodynamic Modeling of Aerospace Vehicles)
  • Article
  • Open Access
26 Citations
8,476 Views
18 Pages

Numerical Continuation of Limit Cycle Oscillations and Bifurcations in High-Aspect-Ratio Wings

  • Andrew J. Eaton,
  • Chris Howcroft,
  • Etienne B. Coetzee,
  • Simon A. Neild,
  • Mark H. Lowenberg and
  • Jonathan E. Cooper

This paper applies numerical continuation techniques to a nonlinear aeroelastic model of a highly flexible, high-aspect-ratio wing. Using continuation, it is shown that subcritical limit cycle oscillations, which are highly undesirable phenomena prev...

(This article belongs to the Special Issue Aeroelasticity)
  • Article
  • Open Access
15 Citations
7,102 Views
15 Pages

The effect of plant-fiber paper or silver nanowires-loaded paper interleaves on the electrical conductivity and interlaminar fracture toughness of composites was studied. Highly conductive paper was prepared by surface-loaded silver nanowires. The pe...

(This article belongs to the Special Issue ECO-COMPASS: Ecological and Multifunctional Composites for Application in Aircraft Interior and Secondary Structures)
  • Article
  • Open Access
21 Citations
9,526 Views
23 Pages

A hybrid reduced-order model for the aeroelastic analysis of flexible subsonic wings with arbitrary planform is presented within a generalised quasi-analytical formulation, where a slender beam is considered as the linear structural dynamics model. A...

(This article belongs to the Special Issue Computational Aerodynamic Modeling of Aerospace Vehicles)
  • Article
  • Open Access
71 Citations
13,382 Views
13 Pages

Natural fiber and wood are environmentally friendly materials with multiscale microstructures. The sound absorption performance of flax fiber and its reinforced composite, as well as balsa wood, were evaluated using the two-microphone transfer functi...

(This article belongs to the Special Issue ECO-COMPASS: Ecological and Multifunctional Composites for Application in Aircraft Interior and Secondary Structures)
  • Review
  • Open Access
18 Citations
10,679 Views
16 Pages

In this review, some major aspects of the current underfill technologies for flip-chip (FC) and fine-pitch-ball-grid-array (FPBGA), including chip-size packaging (CSP), are addressed, with an emphasis on applications, such as aerospace electronics, f...

(This article belongs to the Special Issue Challenges in Reliability Analysis of Aerospace Electronics)
  • Article
  • Open Access
46 Citations
8,686 Views
16 Pages

The spatiotemporal dynamics of the coherent structures in an under-expanded supersonic impinging jet are studied using a spectral proper orthogonal decomposition technique. For this analysis, a large eddy simulation of an under-expanded supersonic im...

(This article belongs to the Special Issue Under-Expanded Jets)
  • Article
  • Open Access
24 Citations
13,636 Views
15 Pages

Why and How to Avoid the Flipped Quaternion Multiplication

  • Hannes Sommer,
  • Igor Gilitschenski,
  • Michael Bloesch,
  • Stephan Weiss,
  • Roland Siegwart and
  • Juan Nieto

Over the last decades quaternions have become a crucial and very successful tool for attitude representation in robotics and aerospace. However, there is a major problem that is continuously causing trouble in practice when it comes to exchanging for...

  • Article
  • Open Access
3 Citations
6,292 Views
16 Pages

Aerothermoelasticity plays a vital role in the design and optimisation of hypersonic aircraft. Furthermore, the transient and nonlinear effects of the harsh thermal and aerodynamic environment a lifting surface is in cannot be ignored. This article i...

(This article belongs to the Special Issue Aeroelasticity)
  • Article
  • Open Access
6 Citations
14,310 Views
17 Pages

The European Aviation Safety Agency (EASA) plans to establish a sole risk-based set of regulations for drones to grant access to European airspace, thus opening a multibillion-euro market. One part of this new regulation set is the so-called “o...

(This article belongs to the Special Issue Civil and Military Airworthiness: Recent Developments and Challenges)
  • Article
  • Open Access
11 Citations
7,148 Views
12 Pages

Autonomous Door and Corridor Traversal with a 20-Gram Flapping Wing MAV by Onboard Stereo Vision

  • Sjoerd Tijmons,
  • Christophe De Wagter,
  • Bart Remes and
  • Guido De Croon

Autonomous flight of Flapping Wing Micro Air Vehicles (FWMAVs) is a major challenge in the field of robotics, due to their light weight and their flapping-induced body motions. An FWMAV is presented weighing a mere 20 g while all its sensors and proc...

(This article belongs to the Special Issue Bio-Inspired Aerospace System)
  • Article
  • Open Access
14 Citations
7,890 Views
20 Pages

The development of an aircraft maintenance planning optimization tool and its application to an aircraft component is presented. Various reliability concepts and approaches have been analyzed, together with objective criteria which can be used to opt...

(This article belongs to the Special Issue Civil and Military Airworthiness: Recent Developments and Challenges)
  • Article
  • Open Access
49 Citations
10,499 Views
7 Pages

Failure Estimates for SiC Power MOSFETs in Space Electronics

  • Kenneth F. Galloway,
  • Arthur F. Witulski,
  • Ronald D. Schrimpf,
  • Andrew L. Sternberg,
  • Dennis R. Ball,
  • Arto Javanainen,
  • Robert A. Reed,
  • Brian D. Sierawski and
  • Jean-Marie Lauenstein

Silicon carbide (SiC) power metal-oxide-semiconductor field effect transistors (MOSFETs) are space-ready in terms of typical reliability measures. However, single event burnout (SEB) due to heavy-ion irradiation often occurs at voltages 50% or lower...

(This article belongs to the Special Issue Challenges in Reliability Analysis of Aerospace Electronics)
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Aerospace - ISSN 2226-4310