AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL-VTOL - Unsteady Lifting Surface Theory in Sonic Flow: The Problem Revisited (TN)
AIAA journal ; 38 , 5 ; 931-932
2000
Article (Journal)
English
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL-VTOL - Swept Thin Wings in Unsteady Sonic Flow (TN)
Online Contents | 2001
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