Transonic and supersonic flow past a 65° delta wing with rounded leading edges : analysis of experimental data
Transsonische und supersonische Strömung an einem 65° -Deltaflügel mit runden Vorderkanten : Analyse experimenteller Ergebnisse
Transsonische und supersonische Strömung an einem 65° -Deltaflügel mit runden Vorderkanten
1988
64 S
Report
English , German
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