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Collection:
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NASA Image eXchange Collection
Collection
NASA Image eXchange Collection
Collection
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Title:
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Drag Reduction Tests on Supersonic Transport Design
Title
Drag Reduction Tests on Supersonic Transport Design
Title
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Description:
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Langley researchers recently completed supersonic tests in the Unitary Plan Wind Tunnel on a nonlinear design for a supersonic transport. Although the drag reduction measured during the tests was not as great as that predicted using computational methods, significant drag reductions were achieved. Future tests will be conducted at a higher Reynolds number, which will be more representative of flight conditions. These tests will be used to identify a supersonic transport configuration that provides maximum drag reduction. Reducing drag decreases operating cost by improving fuel consumption and lowering aircraft weight. As a result, this research has the potential to help make a future high-speed civil transport (HSCT) an affordable means of travel for the flying public.
Description
Langley researchers recently completed supersonic tests in the Unitary Plan Wind Tunnel on a nonlinear design for a supersonic transport. Although the drag reduction measured during the tests was not as great as that predicted using computational methods, significant drag reductions were achieved. Future tests will be conducted at a higher Reynolds number, which will be more representative of flight conditions. These tests will be used to identify a supersonic transport configuration that provides maximum drag reduction. Reducing drag decreases operating cost by improving fuel consumption and lowering aircraft weight. As a result, this research has the potential to help make a future high-speed civil transport (HSCT) an affordable means of travel for the flying public.
Description
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Date:
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08.25.1998
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Credit:
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facet_where:
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Langley Research Center (LaRC)
facet_where
Langley Research Center (LaRC)
facet_where
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facet_when:
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08-25-1998
facet_when
08-25-1998
facet_when
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facet_when_year:
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1998
facet_when_year
1998
facet_when_year
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Media:
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IMAGE
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ID:
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EL-1998-00162
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UID:
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SPD-NIX-EL-1998-0016 2
UID
SPD-NIX-EL-1998-0016 2
UID
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orignial url:
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orignial_url
orignial url
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