A Novel Compression Surface for Integration Design of High Speed Aircraft Forebody and Inlet (AIAA 2015-3618)
AIAA international space planes and hypersonic systems and technologies conference
01.01.2015
14 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Integration Methodology for Waverider-Derived Hypersonic Inlet and Vehicle Forebody (AIAA 2014-3229)
British Library Conference Proceedings | 2014
|British Library Conference Proceedings | 2015
|On the Conceptual Design of Waverider Forebody Geometries (AIAA 2015-1009)
British Library Conference Proceedings | 2015
|DataCite | 1914