IHS ESDU Extrapolating wind-tunnel data to full-scale Reynolds number Part 3: Example (i) Choice of simulation criteria and transition-strip locations for the F4 Wing/Body combination at the design condition 09015

Description
ESDU 09015 illustrates the procedures, detailed in ESDU 07010, which are used to choose aft-fixing locations and CFD extrapolation strategies for low Reynolds number transonic wind-tunnel tests. Tests on the F4 wing/body combination are used as an example.
Description
ESDU 09015 illustrates the procedures, detailed in ESDU 07010, which are used to choose aft-fixing locations and CFD extrapolation strategies for low Reynolds number transonic wind-tunnel tests. Tests on the F4 wing/body combination are used as an example.

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Extrapolating wind-tunnel data to full-scale Reynolds number Part 3: Example (i) Choice of simulation criteria and transition-strip locations for the F4 Wing/Body combination at the design condition - 09015 - IHS ESDU
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Extrapolating wind-tunnel data to full-scale Reynolds number Part 3: Example (i) Choice of simulation criteria and transition-strip locations for the F4 Wing/Body combination at the design condition
09015
Extrapolating wind-tunnel data to full-scale Reynolds number Part 3: Example (i) Choice of simulation criteria and transition-strip locations for the F4 Wing/Body combination at the design condition 09015
ESDU 09015 illustrates the procedures, detailed in ESDU 07010, which are used to choose aft-fixing locations and CFD extrapolation strategies for low Reynolds number transonic wind-tunnel tests. Tests on the F4 wing/body combination are used as an example.

ESDU 09015 illustrates the procedures, detailed in ESDU 07010, which are used to choose aft-fixing locations and CFD extrapolation strategies for low Reynolds number transonic wind-tunnel tests. Tests on the F4 wing/body combination are used as an example.

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Technical Specifications

  IHS ESDU
Product Category Standards and Technical Documents
Product Number 09015
Product Name Extrapolating wind-tunnel data to full-scale Reynolds number Part 3: Example (i) Choice of simulation criteria and transition-strip locations for the F4 Wing/Body combination at the design condition
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