Title: High-speed wind-tunnel tests of a 1/16-scale model of the D-558 research airplane basic longitudinal stability of the D-558-1
Abstract:Report presenting the results of testing on a model of the D-558-1 in order to determine its pitching-moment, lift, and drag characteristics with no nose-inlet flow, and with the tail removed and at a...Report presenting the results of testing on a model of the D-558-1 in order to determine its pitching-moment, lift, and drag characteristics with no nose-inlet flow, and with the tail removed and at a constant setting. Only a limited analysis is provided.Read More
Publication Year: 1948
Publication Date: 1948-05-12
Language: en
Type: article
Access and Citation
AI Researcher Chatbot
Get quick answers to your questions about the article from our AI researcher chatbot