DTIC ADA052541: Investigation of the Boundary Condition at a Wind Tunnel Test Section Wall for a Lifting Wing Body Model at Low Supersonic Speed. Phase 1. Test Preparations, Revision of Computer Program and Exploratory ComputatiReportar como inadecuado



 DTIC ADA052541: Investigation of the Boundary Condition at a Wind Tunnel Test Section Wall for a Lifting Wing Body Model at Low Supersonic Speed. Phase 1. Test Preparations, Revision of Computer Program and Exploratory Computati


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The purpose of this investigation is to study experimentally and theoretically the flow field at locations around a lifting wing-body model, where wind-tunnel walls are normally situated. During Phase 1, which this report covers, the preparations for the experimental investigation have been carried out. The delta-wing-body model, the sting and supp

Autor: Defense Technical Information Center

Fuente: https://archive.org/







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