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 ComputatiReport as inadecuate



 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


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 - Download this document for free, or read online. Document in PDF available to download.

Download or read this book online for free in PDF: 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
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

Author: Defense Technical Information Center

Source: https://archive.org/







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