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Aerospace, Volume 11, Issue 9

September 2024 - 95 articles

Cover Story: Numerical simulations are performed for flows over a circular cylinder at a Reynolds number ranging from 150 to 5000 assess the predictive capability of different turbulence and hybrid RANS-LES models for acoustic wave generation and propagation. In addition, direct numerical simulations (DNS) are utilized to generate validation datasets and to provide more insight into any issues. The DNS predictions demonstrate that noise induced by the vortex shedding is radiated primarily at a 90-degree angle with respect to the wake direction, and it dictates the dominant frequency of the sound pressure waves. Turbulence dominates the noise in the near-field wake, resulting in a broadband pressure spectrum. View this paper
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Articles (95)

  • Article
  • Open Access
1 Citations
2,244 Views
13 Pages

Aerodynamic Drag Coefficient Prediction of a Spike Blunt Body Based on K-Nearest Neighbors

  • Jonathan Arturo Sánchez Muñoz,
  • Christian Lagarza-Cortés and
  • Jorge Ramírez-Cruz

14 September 2024

Spike blunt bodies are a method to reduce drag when a body moves at speeds above sound. Several numerical works based on computational fluid dynamics (CFD) have deeply studied fluid performance and highlighted its advantages. However, most documentat...

  • Article
  • Open Access
3 Citations
2,126 Views
19 Pages

Research on a Honeycomb Structure for Pyroshock Isolation at the Spacecraft–Rocket Interface

  • Xixiong Wang,
  • Zhibo Gao,
  • Dong Cheng,
  • Xuchen Deng,
  • Tao Yu,
  • Zhaoye Qin and
  • Fulei Chu

14 September 2024

Honeycomb is a splendid kind of structure for aerospace engineering with the advantages of light weight, good shock absorption, and good structural stability. This article aims to provide methods to isolate Pyroshocks based on a honeycomb structure a...

  • Article
  • Open Access
4 Citations
2,283 Views
20 Pages

The Dynamic Prediction Method for Aircraft Cabin Temperatures Based on Flight Test Data

  • He Li,
  • Jianjun Zhang,
  • Liangxu Cai,
  • Minwei Li,
  • Yun Fu and
  • Yujun Hao

13 September 2024

For advanced aircraft, the temperature environment inside the cabin is very severe due to the high flight speed and the compact concentration of the electronic equipment in the cabin. Accurately predicting the temperature environment induced inside t...

  • Article
  • Open Access
2 Citations
2,654 Views
15 Pages

13 September 2024

The intricacies of air traffic departure scheduling, especially when numerous flights are delayed, frequently impede the implementation of automated decision-making for scheduling. To surmount this obstacle, a mathematical model is proposed, and a dy...

  • Article
  • Open Access
11 Citations
2,613 Views
18 Pages

13 September 2024

The stratospheric airship, as a near-space vehicle, is increasingly utilized in scientific exploration and Earth observation due to its long endurance and regional observation capabilities. However, due to the complex characteristics of the stratosph...

  • Article
  • Open Access
3,316 Views
17 Pages

Effects of Fuel Penetration on the RDE Performance with JISC Injector Configuration

  • Gyeong-Ui Mo,
  • In-Hoi Koo,
  • Keon-Hyeong Lee,
  • Su-Wan Choi and
  • Jeong-Yeol Choi

13 September 2024

This study investigates the operational characteristics of the Rotating Detonation Engine (RDE), with a focus on fuel injector design. Inspired by the similarity between the fuel injection structure of RDE and the Jet in Supersonic Crossflow (JISC) o...

  • Article
  • Open Access
1 Citations
1,469 Views
19 Pages

13 September 2024

To improve the Solar Array Drive Assembly (SADA) system, a servo control method known as Linear Active Disturbance Rejection Control (LADRC) is introduced, utilizing a speed loop for a Permanent Magnet Synchronous Motor (PMSM). This method serves as...

  • Article
  • Open Access
4 Citations
1,569 Views
21 Pages

12 September 2024

As turbine entry temperatures of modern jet engines continue to increase, additional thermal stresses are introduced onto the high-pressure turbine rotors, which are already burdened by substantial levels of centrifugal and gas loads. Usually, for mo...

  • Article
  • Open Access
1,166 Views
20 Pages

12 September 2024

To accurately analyze the influence of similar weather scenes in the terminal area, a framework is proposed for identifying such scenarios based on the Multiresolution Spatiotemporal Window (MRSTW). The goal is to analyze the impact of similar weathe...

  • Article
  • Open Access
8 Citations
2,548 Views
21 Pages

12 September 2024

Airport noise prediction models are divided into physics-guided methods and data-driven methods. The prediction results of physics-guided methods are relatively stable, but their overall prediction accuracy is lower than that of data-driven methods....

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Aerospace - ISSN 2226-4310