Design of a new supersonic biplane. (October 2020)
- Record Type:
- Journal Article
- Title:
- Design of a new supersonic biplane. (October 2020)
- Main Title:
- Design of a new supersonic biplane
- Authors:
- Zhai, Jian
Zhang, Chen-An
Wang, Fa-Min
Zhang, Wei-Wei - Abstract:
- Abstract: A classic Busemann biplane, consisting of two isosceles-triangle airfoils, can effectively reduce wave-drag and sonic boom in the design condition by correctly placing its lower and upper airfoils. However, its aerodynamic performance dramatically decreases in the off-design conditions due to the flow choking problem. This study presents a new supersonic biplane aiming to produce as low wave-drag as the Busemann biplane in the design condition and to weaken the flow choking problem in the off-design conditions. It places a flat-plate in the middle of the Busemann biplane and removes the upper isosceles-triangle airfoil, so it consists of an isosceles-triangle airfoil and a flat-plate. The design method defines the position between the isosceles-triangle airfoil and the flat-plate as well as the length of the flat-plate by the oblique shock function and Prandtl-Meyer function. In the design condition, the new supersonic biplane has the same wave-cancellation effect as the Busemann biplane. Besides, in the off-design conditions, it also has a weaker flow choking problem due to a higher ratio of the throat area to the inlet area. The numerical results show that it has lower drag, higher lift-to-drag ratio, and is easier to start than the Busemann biplane. Highlights: A new supersonic biplane is developed by replacing the upper airfoil of the Busemann biplane with a flat-plate. In the design condition, the new supersonic biplane has as low wave-drag as the BusemannAbstract: A classic Busemann biplane, consisting of two isosceles-triangle airfoils, can effectively reduce wave-drag and sonic boom in the design condition by correctly placing its lower and upper airfoils. However, its aerodynamic performance dramatically decreases in the off-design conditions due to the flow choking problem. This study presents a new supersonic biplane aiming to produce as low wave-drag as the Busemann biplane in the design condition and to weaken the flow choking problem in the off-design conditions. It places a flat-plate in the middle of the Busemann biplane and removes the upper isosceles-triangle airfoil, so it consists of an isosceles-triangle airfoil and a flat-plate. The design method defines the position between the isosceles-triangle airfoil and the flat-plate as well as the length of the flat-plate by the oblique shock function and Prandtl-Meyer function. In the design condition, the new supersonic biplane has the same wave-cancellation effect as the Busemann biplane. Besides, in the off-design conditions, it also has a weaker flow choking problem due to a higher ratio of the throat area to the inlet area. The numerical results show that it has lower drag, higher lift-to-drag ratio, and is easier to start than the Busemann biplane. Highlights: A new supersonic biplane is developed by replacing the upper airfoil of the Busemann biplane with a flat-plate. In the design condition, the new supersonic biplane has as low wave-drag as the Busemann biplane. In the off-design conditions, the new supersonic biplane has a weaker flow choking problem. … (more)
- Is Part Of:
- Acta astronautica. Volume 175(2020)
- Journal:
- Acta astronautica
- Issue:
- Volume 175(2020)
- Issue Display:
- Volume 175, Issue 2020 (2020)
- Year:
- 2020
- Volume:
- 175
- Issue:
- 2020
- Issue Sort Value:
- 2020-0175-2020-0000
- Page Start:
- 216
- Page End:
- 233
- Publication Date:
- 2020-10
- Subjects:
- Busemann biplane -- Supersonic/hypersonic aircraft -- Wave-cancellation -- Flow choking
Astronautics -- Periodicals
Outer space -- Exploration -- Periodicals
Astronautics
Periodicals
629.405 - Journal URLs:
- http://www.sciencedirect.com/science/journal/00945765 ↗
http://www.elsevier.com/journals ↗ - DOI:
- 10.1016/j.actaastro.2020.05.010 ↗
- Languages:
- English
- ISSNs:
- 0094-5765
- Deposit Type:
- Legaldeposit
- View Content:
- Available online (eLD content is only available in our Reading Rooms) ↗
- Physical Locations:
- British Library DSC - 0596.750000
British Library DSC - BLDSS-3PM
British Library HMNTS - ELD Digital store - Ingest File:
- 13962.xml