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 experiments
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
Aircraft Engineering and Aerospace Technology: An International Journal (2023) 95 (7): 1081–1091.
Published: 26 April 2023
... 2022 18 01 2023 09 02 2023 © Emerald Publishing Limited 2023 Emerald Publishing Limited Licensed re-use rights only Vortices Flow separation Pitching moment coefficient Wind tunnel experiments CFD Blunt leading-edge contour MULDICON wing Wind tunnel testing...
Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (2023) 95 (1): 1–13.
Published: 01 June 2022
... the effects of a heatwave over an airfoil. Then, the numerical simulations and wind tunnel experiments are conducted. Findings The numerical and wind tunnel’s experimental investigations have been performed on a 2D airfoil under a heatwave environment, i.e. 27ºC, 40ºC and 50ºC for different flight...
Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (2020) 92 (8): 1125–1131.
Published: 13 June 2020
... is used. Wind tunnel experiments were conducted at the chord-based Reynolds number of Rec = 1.6 × 105 to validate the aerodynamic characteristics over SS007 airfoil. Findings The numerical results revealed that the LSB characteristics of a SS007 airfoil...
