Engineering

AeroCalculator

Authors

DOI:

https://doi.org/10.71107/fe334392

Abstract

AeroCalculator is a free, browser-based tool for the aerodynamic and gas-dynamic calculations that arise in supersonic and hypersonic vehicle design, CFD pre-processing, and propulsion analysis. It implements 22 self-contained modules across the US Standard Atmosphere, normal / oblique / conical shock relations, Prandtl-Meyer expansion, Fay-Riddell stagnation heat flux, Chapman-Jouguet detonation, the Kantrowitz inlet limit, and more. All numerical engines have been cross-verified against Anderson's Modern Compressible Flow appendices, NACA Report 1135, the Sims cone tables, and the US Standard Atmosphere 1976.

Use the web version of AeroCalculator:

https://iconclusions.com/aerocalculator/

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Author Biography

  • Omer Musa, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, People’s Republic of China

    College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, People’s Republic of China 

References

AeroCalculator

Downloads

Published

2026-05-20

Issue

Vol. 1 No. 2 (2025): Conclusions in Engineering

Section

Articles

License

Copyright (c) 2025 Omer Musa (Author)

Creative Commons License

This work is licensed under a Creative Commons Attribution 4.0 International License.

How to Cite

AeroCalculator. (2026). Conclusions in Engineering, 1(2). https://doi.org/10.71107/fe334392

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