CONTENTS
Volume 10, Number 5, 2023
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Aircraft delivery vehicle with fuzzy time window for improving search algorithm
C.C. Hung, T. Nguyễn and C.Y. Hsieh
pages 393-418.
DOI: 10.12989/aas.2023.10.5.393
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Aeroelastic stability analysis of a two-stage axially deploying telescopic wing with rigid-body motion effects
Sayed Hossein Moravej Barzani and Hossein Shahverdi
pages 419-437.
DOI: 10.12989/aas.2023.10.5.419
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Frequency analysis of liquid sloshing in prolate spheroidal containers and comparison with aerospace spherical and cylindrical tanks
Mohammad Mahdi Mohammadi, Hojat Taei, Hamid Moosazadeh and Mohammad Sadeghi
pages 439-455.
DOI: 10.12989/aas.2023.10.5.439
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Computation of aerodynamic coefficients of a re-entry vehicle at Mach 6
R.C. Mehta and E. Rathakrishnan
pages 457-471.
DOI: 10.12989/aas.2023.10.5.457
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A method to analyze the flyability of airplane trajectories with specified engine power
Gilles Labonté, Vincent Roberge and Mohammed Tarbouchi
pages 473-494.
DOI: 10.12989/aas.2023.10.5.473