A Web-based version of the aircraft design program ACSYNT has been created. “Web-ACSYNT” provides the user with a familiar user interface and is accessible from multiple platforms. Analyses are based upon a set of baseline aircraft models which can be modified through a carefully selected set of parameters related to weight, aerodynamics, propulsion, economics, and mission. The software is intended to become one of the models that comprise the Aviation System Analysis Capability (ASAC) currently being developed by NASA under the Advanced Subsonic Technology (AST) program.
“Web-ACSYNT”: Conceptual-Level Aircraft Systems Analysis on the Internet
Sae Technical Papers
World Aviation Congress & Exposition ; 1997
1997-10-01
Aufsatz (Konferenz)
Englisch
Improving Aircraft Conceptual Design Tools - New Enhancements to ACSYNT
British Library Conference Proceedings | 1993
|Putting the ACSYNT on Aircraft Design
British Library Online Contents | 1994
|Overview of ACSYNT for Light Aircraft Design
SAE Technical Papers | 1995
|