A Hypersonic Strike Fighter (HSF) would provide many benefits over current fighters, including increased effectiveness and survivability. However, there are many design challenges to developing such a vehicle. Therefore the conceptual design of an HSF requires the development of new tools and methods to analyze and select vehicle concepts. A parametric method was developed to determine aerodynamic characteristics of hypersonic vehicles in a rapid, automated way. This parametric method and other tools were then used to select a baseline design and optimize this baseline for the notional mission.
Implementation of Parametric Anaylsis to the Aerodynamic Design of a Hypersonic Strike Fighter
Sae Technical Papers
World Aviation Congress & Exposition ; 2000
10.10.2000
Aufsatz (Konferenz)
Englisch
Implementation of Parametric Anaylsis to the Aerodynamic Design of a Hypersonic Strike Fighter
British Library Conference Proceedings | 2000
|NTRS
|Online Contents | 1998
Online Contents | 1997