Analysis of stagger effects on Busemann supersonic biplane airfoil in shock tube tests by point diffraction interferometer method-Reference-Cited by-同舟云学术

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Analysis of stagger effects on Busemann supersonic biplane airfoil in shock tube tests by point diffraction interferometer method

Published:2022-12 Issue: Volume:131 Page:107957
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Nguyen T.D.^ORCID,Taguchi M.,Tsuji K.,Kashitani M.,Tanno H.,Kusunose K.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference30 articles.

1. Low-boom low-drag optimization in a multidisciplinary design analysis optimization environment;Sun;Aerosp. Sci. Technol.,2019

2. Aerodynamic Design of Supersonic Biplane, Cutting Edge and Related Topics; the 21st Century COE Program; International COE of Flow Dynamic Lecture Series;Kusunose,2007

3. Supersonic biplane–a review;Kusunose;Prog. Aerosp. Sci.,2011

4. Wind tunnel testing on start/unstart characteristics of finite supersonic biplane wing;Yamashita;Int. J. Aerosp. Eng.,2013

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