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Aerospace, Volume 11, Issue 10

2024 October - 76 articles

Cover Story: In recent decades, the problem of pollution related to human activities has pushed research towards zero or net-zero carbon solutions for transportation. The main objective of this paper is to perform a preliminary performance assessment of the use of hydrogen in conventional turbine engines for aeronautical applications. A 0-D dynamic model of the Allison 250 C-18 turboshaft engine was designed in the MATLAB/Simulink environment. The model was dimensioned based on the parameters measured during the testing campaign and validated by the acquired data using Jet A-1 fuel. Further, the 0-D dynamic engine model was used to predict the performance of the engine, using hydrogen as the input of the theoretical combustion model. The simulation’s outputs running conventional Kerosene Jet A-1 and hydrogen and using different throttle profiles were compared. View this paper
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Articles (76)

  • Article
  • Open Access
3 Citations
2,833 Views
23 Pages

20 October 2024

As the value and importance of urban air mobility (UAM) are being recognized, there is growing attention towards UAM. To ensure that urban air traffic can serve passengers to the greatest extent while ensuring safety and generating revenue, there is...

  • Article
  • Open Access
1 Citations
7,632 Views
39 Pages

18 October 2024

Recent developments in aircraft electrical technology, such as the design and production of more electric aircraft (MEA) and major steps in the development of all-electric aircraft (AEA), have had a significant impact on aircraft’s electrical p...

  • Article
  • Open Access
1,245 Views
25 Pages

Position Normalization of Propellant Grain Point Clouds

  • Junchao Wang,
  • Fengnian Tian,
  • Renfu Li,
  • Zhihui Li,
  • Bin Zhang and
  • Xuelong Si

18 October 2024

Point cloud data obtained from scanning propellant grains with 3D scanning equipment exhibit positional uncertainty in space, posing significant challenges for calculating the relevant parameters of the propellant grains. Therefore, it is essential t...

  • Article
  • Open Access
1 Citations
1,966 Views
18 Pages

An Online Data-Driven Method for Accurate Detection of Thermal Updrafts Using SINDy

  • Yufeng Lu,
  • Chenglou Liu,
  • Haichao Hong,
  • Yunwei Huang,
  • Tingwei Ji and
  • Fangfang Xie

18 October 2024

Utilizing thermal updrafts shows potential for enabling long-endurance cruising of fixed-wing unmanned aerial vehicles without energy consumption. This article presents a novel online method based on sparse identification of nonlinear dynamics (SINDy...

  • Article
  • Open Access
2 Citations
3,059 Views
21 Pages

Noise Study Auralization of an Open-Rotor Engine

  • Qing Zhang,
  • Siyi Jiang,
  • Xiaojun Yang,
  • Yongjia Xu and
  • Maosheng Zhu

17 October 2024

Based on the performance and acoustic data files of reduced-size open-rotor engines in low-speed wind tunnels, the static sound pressure level was derived by converting the 1-foot lossless spectral density into sound-pressure-level data, the backgrou...

  • Article
  • Open Access
2 Citations
1,579 Views
18 Pages

17 October 2024

High-speed ballistic impact tests were conducted at room temperature and 500 °C on nickel-based superalloy GH4169 simulated blade specimens containing leading-edge features. The microscopic characteristics of the impact notch at room temperature...

  • Article
  • Open Access
1 Citations
1,656 Views
12 Pages

16 October 2024

A partial space elevator (PSE) is a multi-body tethered space system in which the main satellite, typically an ultra-large spacecraft or a space station in a higher orbit, is connected to a transport spacecraft in a lower orbit via a tether, maintain...

  • Article
  • Open Access
7 Citations
2,853 Views
23 Pages

16 October 2024

Laser powder bed fusion (LPBF) is one of the high-precision additive manufacturing techniques for producing complex 3D components. It is well known that defects appear in additive-manufactured parts, and they deeply affect the fatigue properties; eve...

  • Article
  • Open Access
5 Citations
1,552 Views
24 Pages

16 October 2024

The self-circulating casing treatment can effectively expand the stable working range of the compressor, with little impact on its efficiency. With a single-stage transonic axial flow compressor NASA (National Aeronautics and Space Administration) St...

  • Article
  • Open Access
4 Citations
3,335 Views
17 Pages

16 October 2024

Fan blade icing can affect efficiency and aerodynamic stability, and the shed ice may be sucked into the core of the engine, causing adverse effects or even damage to the compressor components. Ice accretion and shedding are among the key issues in e...

  • Article
  • Open Access
2 Citations
1,298 Views
19 Pages

15 October 2024

The foldable tail of the box-type launch vehicle poses a risk of mechanical jamming during the launch process, which is not conducive to the smooth completion of the flight mission. The integrated nonfolding ducted tail proposed in this article can s...

  • Article
  • Open Access
1 Citations
1,459 Views
14 Pages

15 October 2024

A numerical simulation of an unsteady gas flow containing inert solid particles in a shock tube is carried out using the interpenetrating continuum model. The gas and dispersed phases are characterized by governing equations that express the concepts...

  • Article
  • Open Access
3 Citations
2,211 Views
18 Pages

Precision Manufacturing in China of Replication Mandrels for Ni-Based Monolithic Wolter-I X-ray Mirror Mandrels

  • Jiadai Xue,
  • Bo Wang,
  • Qiuyan Liao,
  • Kaiji Wu,
  • Yutao Liu,
  • Yangong Wu,
  • Wentao Chen,
  • Zheng Qiao,
  • Yuan Jin and
  • Yong Chen
  • + 5 authors

15 October 2024

The X-ray satellite “Einstein Probe” of the Chinese Academy of Sciences (CAS) was successfully launched on 9 January 2024 at 15:03 Beijing Time from the Xichang Satellite Launch Center in China with a “Long March-2C” rocket. T...

  • Article
  • Open Access
4,034 Views
15 Pages

15 October 2024

According to the requirements of the small double-pulse solid rocket motor, a compartmentalized isolation device has been designed. This device consists of a metal diaphragm and a support frame. An experimental study and numerical simulation were use...

  • Article
  • Open Access
1 Citations
1,682 Views
13 Pages

15 October 2024

In this paper, the flow characteristics of a continuous-type liquid–liquid pintle injector are described, focusing on the differential impact of a non-uniform center-flow distribution on single- and bi-injection methodologies as well as the cav...

  • Article
  • Open Access
4 Citations
2,993 Views
22 Pages

14 October 2024

Advanced airborne power generation technology represents one of the most effective solutions for meeting the electricity requirements of hypersonic vehicles during long-endurance flights. This paper proposes a power generation system that integrates...

  • Article
  • Open Access
3 Citations
1,559 Views
16 Pages

14 October 2024

In the realm of autonomous aerial refueling missions for unmanned aerial vehicles (UAVs), the controllable drogue represents a novel approach that significantly enhances both the safety and efficiency of aerial refueling operations. This paper delves...

  • Article
  • Open Access
1 Citations
2,002 Views
30 Pages

13 October 2024

For civil high-speed rotorcraft designed to operate at specific cruising altitudes, this study proposes nine structural design schemes for pressurized cabins. These schemes integrate commonly used materials and processing technologies in the aviation...

  • Article
  • Open Access
2 Citations
1,838 Views
20 Pages

12 October 2024

The rapid growth of the aviation industry highlights the need for strong safety management. Analyzing data on unsafe aviation events is crucial for preventing risks. This paper presents a new method that integrates the Transformer network model, clus...

  • Article
  • Open Access
3 Citations
3,245 Views
25 Pages

12 October 2024

In the 21st century, mega-constellations and interconnected satellite constellations deployed at various orbital altitudes, such as LEO, MEO, and GEO, with low Earth orbits (LEOs) being the most commonly used, have emerged as a trend, aiming to enhan...

  • Article
  • Open Access
1 Citations
1,678 Views
16 Pages

Crack Growth Analytical Model Considering the Crack Growth Resistance Parameter Due to the Unloading Process

  • Guo Li,
  • Shuchun Huang,
  • Zhenlei Li,
  • Wanqiu Lu,
  • Shuiting Ding,
  • Rong Chen and
  • Fan Cao

12 October 2024

Crack growth analysis is essential for probabilistic damage tolerance assessment of aeroengine life-limited parts. Traditional crack growth models directly establish the stress ratio–crack growth rate or crack opening stress relationship and fo...

  • Article
  • Open Access
1 Citations
2,408 Views
15 Pages

11 October 2024

Wake vortices generated by aircraft during near-ground operations have a significant impact on airport safety during takeoffs and landings. Identifying wake vortices in complex airspaces assists air traffic controllers in making informed decisions, e...

  • Article
  • Open Access
1 Citations
1,489 Views
22 Pages

Pulsar Signal Adaptive Surrogate Modeling

  • Tomáš Kašpárek and
  • Peter Chudý

11 October 2024

As the number of spacecraft heading beyond Earth’s orbit increased in recent years, autonomous navigation solutions have become increasingly important. One such solution is pulsar-based navigation. The availability of pulsar signals for simulat...

  • Article
  • Open Access
1 Citations
1,956 Views
19 Pages

State Analysis and Emergency Control of Planetary Rover with Faulty Drive Wheel

  • Zhicheng Jia,
  • Jingfu Jin,
  • Xinju Dong,
  • Yingchun Qi,
  • Meng Zou and
  • Qingyu Yu

11 October 2024

Wheel failure is one of the worst problems for a planetary rover working on Mars or the Moon, which may lead to the interruption of the exploration mission and even the loss of mobility. In this study, a driving test of a planetary rover prototype wi...

  • Article
  • Open Access
7 Citations
1,938 Views
24 Pages

11 October 2024

There are massive amounts of civil aviation safety oversight reports collected each year in the civil aviation of China. The narrative texts of these reports are typically short texts, recording the abnormal events detected during the safety oversigh...

  • Article
  • Open Access
3 Citations
2,908 Views
23 Pages

11 October 2024

To achieve higher thermal efficiency in a gas turbine, increasing the turbine inlet temperature is necessary. The rotor blade at the first stage tolerates the highest temperature, and the serpentine internal channel located in the middle chord of the...

  • Article
  • Open Access
4 Citations
1,643 Views
11 Pages

10 October 2024

To understand the asymmetric flow of a slender body with low-aspect ratio fins, a wind tunnel experiment was carried out, and the asymmetric flow was observed when the pair of fins had a symmetric deflection angle of 30° at a small angle of attac...

  • Article
  • Open Access
3 Citations
1,582 Views
22 Pages

10 October 2024

Low-frequency harmonic interference is an important factor that affects the performance of low-speed direct-drive servo systems. In order to improve the low-speed smoothness of direct-drive servo, firstly, the causes of the first and second harmonics...

  • Article
  • Open Access
3,185 Views
13 Pages

Variations in Heart Rate Variability and Physiological Responses during Analog Space Missions: An Exploratory Study

  • Acatzin Benítez-Salgado,
  • Miguel Ángel Peña-Castillo,
  • Laura Mercedes Santiago-Fuentes,
  • Luis Adrián Zúñiga-Avilés,
  • Eric Alonso Abarca-Castro,
  • Ana Karen Talavera-Peña,
  • Lizeth Avila-Gutierrez,
  • Jorge Rodríguez-Arce and
  • José Javier Reyes-Lagos

10 October 2024

This exploratory study investigates changes in the autonomic cardiac system of young analog astronauts in a hostile, confined, and isolated environment. It uses linear and nonlinear indices of heart rate variability (HRV) during a Mars analog mission...

  • Article
  • Open Access
2 Citations
1,556 Views
19 Pages

10 October 2024

This paper examines the atomization characteristics of liquid hydrogen fuel in a premixing tube under different operating conditions. Hydrogen fuel’s unique injection morphology and atomization behavior were analyzed using the Volume of Fluid-t...

  • Article
  • Open Access
1 Citations
1,771 Views
22 Pages

Research on Chip Removal Performance of Rotary Percussive Ultrasonic Drill for Planetary Rock Sampling

  • Yinchao Wang,
  • Dongdong Zheng,
  • Zihao Yin,
  • Weiwei Zhang,
  • Lin Zu,
  • Guanghong Tao and
  • Suyang Yu

9 October 2024

The objective of the kinematic model of rock chips is to examine the impact of the driving parameters of drilling tools on the effective chip removal speed, with a view to analyze the chip removal performance of rotary percussion ultrasonic drilling....

  • Article
  • Open Access
4 Citations
2,090 Views
23 Pages

9 October 2024

Advanced Aerial Mobility (AAM) platforms are poised to begin high-density operations in urban areas nationwide. This new category of aviation platforms spans a broad range of sizes, from small package delivery drones to passenger-carrying vehicles. U...

  • Article
  • Open Access
1 Citations
1,223 Views
15 Pages

9 October 2024

Taking a four-stage transonic compressor as the research object, the Lagrange particle tracking method was used to simulate the multiphase flow by considering the particle fragmentation, collision and evaporation models, and the influence of differen...

  • Article
  • Open Access
1,334 Views
27 Pages

9 October 2024

This paper proposes a pose control scheme of for proximity maneuvering for tracking and observing noncooperative targets with unknown acceleration, which is an important prerequisite for on-orbit operations in space. It mainly consists of a finite-ti...

  • Article
  • Open Access
3 Citations
2,295 Views
18 Pages

9 October 2024

This article examines the flight dynamics and trajectory analysis of a parachute–payload system deployed from a C-17 aircraft. The aircraft is modeled with an open cargo door, extended flaps, and four turbo-fan engines operating at an altitude...

  • Article
  • Open Access
3 Citations
2,880 Views
11 Pages

9 October 2024

(1) Background: As the principal structural element of an unmanned aerial vehicle (UAV), a lightweight, high-performance wing-fuselage connection structure plays an important role in UAV structural integrity. Previous studies focused on the static st...

  • Article
  • Open Access
1,390 Views
18 Pages

8 October 2024

Blade slotting technology is an effective measure to improve the flow structure on the suction surface of a blade and enhance the performance of turbomachinery. To investigate the impact of various slot sizes on the flow field of a single-stage trans...

  • Article
  • Open Access
4 Citations
4,227 Views
33 Pages

Liquid Rocket Engine Performance Characterization Using Computational Modeling: Preliminary Analysis and Validation

  • Md. Amzad Hossain,
  • Austin Morse,
  • Iram Hernandez,
  • Joel Quintana and
  • Ahsan Choudhuri

8 October 2024

The need to refuel future missions to Mars and the Moon via in situ resource utilization (ISRU) requires the development of LOX/LCH4 engines, which are complex and expensive to develop and improve. This paper discusses how the use of digital engineer...

  • Article
  • Open Access
1 Citations
1,492 Views
19 Pages

Study on the Influence of Tip Clearance on Working Characteristics of High-Altitude Fan

  • Wei Qu,
  • Xiaohui He,
  • Chunlian Duan,
  • Yumei Qin,
  • Zeqing He and
  • Yanchu Yang

8 October 2024

To study the influence of tip clearance on the working characteristics of high-altitude fans, this paper takes the MIX-140 high-altitude fan as the research object. Five different tip clearance (TC) models are selected. The CFD method is used to anal...

  • Article
  • Open Access
13 Citations
5,352 Views
19 Pages

8 October 2024

A four-dimensional (4D) trajectory is a multi-dimensional time series that embodies rich spatiotemporal features. However, its high complexity and inherent uncertainty pose significant challenges for accurate prediction. In this paper, we present a n...

  • Review
  • Open Access
8 Citations
6,598 Views
30 Pages

8 October 2024

With the increasing adoption of composite materials in aircraft construction, traditional anti-icing technologies face significant challenges due to the low thermal conductivity and heat resistance of composite resins. These limitations have spurred...

  • Article
  • Open Access
2 Citations
3,184 Views
12 Pages

Optimal Design of High Specific Power Electric Machines for Fully Electric Regional Aircraft: A Case Study of 1MW S-PMSM

  • Taha El Hajji,
  • Ahmed Hemeida,
  • Antti Lehikoinen,
  • Floran Martin and
  • Anouar Belahcen

8 October 2024

The aviation industry is undergoing electrification due to the increased global focus on reducing emissions in air traffic. Regarding the volatility of raw material prices, one main objective is the increase in the specific power of the motor. This m...

  • Article
  • Open Access
2 Citations
2,331 Views
18 Pages

7 October 2024

A numerical method has been presented to simulate hypervelocity impacts on metal targets. The target is a rectangular prism and is positioned at various inclined angles relative to the impact direction, while four different projectiles such as square...

  • Article
  • Open Access
2 Citations
3,586 Views
20 Pages

Shock Wave and Aeroelastic Coupling in Overexpanded Nozzle

  • Haifeng Hu,
  • Xinni Gao,
  • Yushan Gao and
  • Jianwen Yang

7 October 2024

The growing demand for increasing the engine power of a liquid rocket is driving the development of high-power De-Laval nozzles, which is primarily achieved by increasing the expansion ratio. A high-expansion-ratio for De-Laval nozzles can cause flow...

  • Article
  • Open Access
2 Citations
2,061 Views
24 Pages

6 October 2024

The geometric correction of thermal infrared (TIR) orthophotos generated by unmanned aerial vehicles (UAVs) presents significant challenges due to low resolution and the difficulty of identifying ground control points (GCPs). This study addresses the...

  • Article
  • Open Access
2 Citations
2,212 Views
26 Pages

0-D Dynamic Performance Simulation of Hydrogen-Fueled Turboshaft Engine

  • Mattia Magnani,
  • Giacomo Silvagni,
  • Vittorio Ravaglioli and
  • Fabrizio Ponti

6 October 2024

In the last few decades, the problem of pollution resulting from human activities has pushed research toward zero or net-zero carbon solutions for transportation. The main objective of this paper is to perform a preliminary performance assessment of...

  • Article
  • Open Access
2 Citations
2,414 Views
15 Pages

6 October 2024

In this study, stall flutter onset prediction in a transonic compressor is carried out using the (uncoupled) energy method with Fourier transform. As the study is conducted computationally using computational fluid dynamics (CFD)-based simulations, t...

  • Article
  • Open Access
1 Citations
1,674 Views
19 Pages

Stress Analysis of Ice Layers on Fan Rotor Blades in Aeroengines

  • Zhiyuan Xu,
  • Lifen Zhang,
  • Hailong Guo and
  • Zhenxia Liu

6 October 2024

Fan rotor blades are critical components of aeroengines. When an aircraft flies in icing conditions, ice accumulation on the fan surface may lead to periodic shedding. Severe ice shedding can cause mechanical damage to the engine, posing significant...

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Aerospace - ISSN 2226-4310