Stochastic optimization of high-altitude airship envelopes based on kriging method

Author:

García-Gutiérrez AdriánORCID,Gonzalo JesúsORCID,Domínguez Diego,López Deibi

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference54 articles.

1. On the capabilities and limitations of high altitude pseudo-satellites;Gonzalo;Prog. Aerosp. Sci.,2018

2. Towards the advent of high-altitude pseudo-satellites (haps);Kirsch,2019

3. Shape optimization and experimental research of near space airship;Ma;Proc. Inst. Mech. Eng., Part G, J. Aerosp. Eng.,2019

4. Shape optimization of near-space airships considering the effect of the propeller;Li;J. Aerosp. Eng.,2020

5. A study on the aerodynamic characteristics of a stratospheric airship in its entire flight envelope;Sun;Proc. Inst. Mech. Eng., Part G, J. Aerosp. Eng.,2018

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