Update search
Filter
- All
- Title
- Author
- Author Affiliations
- Full Text
- Abstract
- Keyword
- DOI
- ISBN
- EISBN
- ISSN
- EISSN
- Issue
- Volume
- References
Filter
- All
- Title
- Author
- Author Affiliations
- Full Text
- Abstract
- Keyword
- DOI
- ISBN
- EISBN
- ISSN
- EISSN
- Issue
- Volume
- References
Filter
- All
- Title
- Author
- Author Affiliations
- Full Text
- Abstract
- Keyword
- DOI
- ISBN
- EISBN
- ISSN
- EISSN
- Issue
- Volume
- References
Filter
- All
- Title
- Author
- Author Affiliations
- Full Text
- Abstract
- Keyword
- DOI
- ISBN
- EISBN
- ISSN
- EISSN
- Issue
- Volume
- References
Filter
- All
- Title
- Author
- Author Affiliations
- Full Text
- Abstract
- Keyword
- DOI
- ISBN
- EISBN
- ISSN
- EISSN
- Issue
- Volume
- References
Filter
- All
- Title
- Author
- Author Affiliations
- Full Text
- Abstract
- Keyword
- DOI
- ISBN
- EISBN
- ISSN
- EISSN
- Issue
- Volume
- References
NARROW
Format
Journal
Type
Date
Availability
1-3 of 3
Keywords: Wind tunnel test
Close
Follow your search
Access your saved searches in your account
Would you like to receive an alert when new items match your search?
Sort by
Journal Articles
Juan Manuel Bustamante Alarcon, Jose Leonel Sanchez Marmolejo, Eduardo Steed Espinoza Quesada, Carlos Santana Delgado, Octavio Garcia-Salazar, Carlos Amir Escalante-Velázquez
Aircraft Engineering and Aerospace Technology: An International Journal (2025) 97 (4): 456–465.
Published: 04 April 2025
... for transition, adding a step at the bottom to improve fixed-wing performance. Wind tunnel tests showed a 66% improvement in the Lift-to-Drag ratio with a step design. Similarly, Ying-Jie Guan and Lee (2023) proposed an H-VTOL design with tilted ducted-fans, where computational fluid dynamics (CFD) simulations...
Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (2020) 92 (7): 973–979.
Published: 28 May 2020
... including wingtip, slat and flap loss were considered. The numerical simulations were performed with ANSYS Fluent. The computational fluid dynamics calculation was validated by wind tunnel tests. Findings The aerodynamic performance of the aircraft with wing-damaged condition was presented...
Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (2013) 85 (4): 316–325.
Published: 28 June 2013
... The designed contra‐rotating propeller can be used in fixed wing aeroplane if torque equal to zero is required. Originality/value Original design of the balance is described for the first time, as well as test procedures applied in this experiment. Most of wind tunnel test results are also new and never...
