Predictor corrector algorithms considering multiple constraints for entry vehicles.
- Published in:
- Aeronautical Journal, 2022, v. 126, n. 1305, p. 1874, doi. 10.1017/aer.2022.19
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- Publication type:
- Article
Works matching IS 00019240 AND DT 2022 AND VI 126 AND IP 1305
Results: 7
1
2
Steady and unsteady aerodynamic loading of a NACA 16-616 aerofoil in a uniform flow.
- Published in:
- Aeronautical Journal, 2022, v. 126, n. 1305, p. 1897, doi. 10.1017/aer.2022.66
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- Article
3
Accuracy of Küchemann's prediction for the locus of aerodynamic centres on swept wings compared to an inviscid panel method.
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- Aeronautical Journal, 2022, v. 126, n. 1305, p. 1853, doi. 10.1017/aer.2022.34
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- Publication type:
- Article
4
Single channel digital controller design for a high spinning rate rolling airframe missile.
- Published in:
- Aeronautical Journal, 2022, v. 126, n. 1305, p. 1815, doi. 10.1017/aer.2022.30
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- Publication type:
- Article
5
Analysis and modelling of airport resilience, robustness, and vulnerability: impact of COVID-19 pandemic disease.
- Published in:
- Aeronautical Journal, 2022, v. 126, n. 1305, p. 1924, doi. 10.1017/aer.2022.25
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- Publication type:
- Article
6
Embedded magnetorquer for the more demanding multi-cube small satellites.
- Published in:
- Aeronautical Journal, 2022, v. 126, n. 1305, p. 1954, doi. 10.1017/aer.2022.24
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- Publication type:
- Article
7
Transonic small disturbance unsteady potential flow over very high aspect ratio wings.
- Published in:
- Aeronautical Journal, 2022, v. 126, n. 1305, p. 1834, doi. 10.1017/aer.2022.5
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- Publication type:
- Article