Next-Generation Aerodynamics for High-Performance Aircraft and Space Launch Vehicles

This paper looks at the progress of aerodynamic tech on high-performance aircraft and space launch vehicles. It uses new aerodynamic ‎designs, CFD models, and experimental testing to advance aviation and space exploration. It examines pilots' challenges in atmospheric and ‎space launches, prioritizing high-speed airflow in supersonic and hypersonic conditions. Research tackles drag control, heat dissipation, and ‎aerodynamic stability to optimize aircraft performance at high speeds. Modern materials like lightweight composites and heat-resistant ‎coatings are featured in the article to improve operational durability and performance. The article discussed adaptive surface control systems ‎capable of morphing a wing's shape during flight to enhance lift and minimize drag. This allows for improved maneuverability, increased ‎fuel efficiency, and better mission accomplishment metrics. By using computational fluid dynamics (CFD), one can limit empirical testing ‎for a given research problem. The integration of new materials and technological advances in aviation and aerospace results in significant ‎performance advances while also achieving sustainable operations.

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Publication Details

Journal
International Journal of Basic and Applied Sciences
Published
2025-10-31
DOI
https://doi.org/10.14419/v1v7qw20
Primary Topic
Plasma and Flow Control in Aerodynamics
Type
article
Field-Weighted Citation Impact
0.00
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article

Next-Generation Aerodynamics for High-Performance Aircraft and Space Launch Vehicles

Sayanti Benerjee, F. Rahman, Ghorpade Bipin Shivaji
International Journal of Basic and Applied Sciences
Plasma and Flow Control in Aerodynamics
article

Next-Generation Aerodynamics for High-Performance Aircraft and Space Launch Vehicles

Sayanti Benerjee, F. Rahman, Ghorpade Bipin Shivaji
article en

Abstract

This paper looks at the progress of aerodynamic tech on high-performance aircraft and space launch vehicles. It uses new aerodynamic ‎designs, CFD models, and experimental testing to advance aviation and space exploration. It examines pilots' challenges in atmospheric and ‎space launches, prioritizing high-speed airflow in supersonic and hypersonic conditions. Research tackles drag control, heat dissipation, and ‎aerodynamic stability to optimize aircraft performance at high speeds. Modern materials like lightweight composites and heat-resistant ‎coatings are featured in the article to improve operational durability and performance. The article discussed adaptive surface control systems ‎capable of morphing a wing's shape during flight to enhance lift and minimize drag. This allows for improved maneuverability, increased ‎fuel efficiency, and better mission accomplishment metrics. By using computational fluid dynamics (CFD), one can limit empirical testing ‎for a given research problem. The integration of new materials and technological advances in aviation and aerospace results in significant ‎performance advances while also achieving sustainable operations.

International Journal of Basic and Applied SciencesVol. 14(SI-1)
International Management Institute (IN), Kalinga University (IN)
Openalex Percentile: Top 56%
Plasma and Flow Control in Aerodynamics
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