Integration of Aerodynamic, Structural, Cost and Manufacturing Considerations During the Conceptual Design of a Thrust Reverser Cascade

Research output: Contribution to conferencePaper

9 Citations (Scopus)
Original languageEnglish
Pages1-12
Number of pages12
Publication statusPublished - Jan 2004
EventAIAA Aerospace Conference - Reno, Nevada, United States
Duration: 01 Jan 200401 Jan 2004

Conference

ConferenceAIAA Aerospace Conference
CountryUnited States
CityReno, Nevada
Period01/01/200401/01/2004

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