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AERION CORP
US14 patents
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US7837142B2Nov 23, 2010
Supersonic aircraft jet engine
AERION CORP20 citations89
US10724472B1Jul 28, 2020
High flow plug nozzle apparatus and method of using the same
AERION CORP18 citations84
US7004428B2Feb 28, 2006
Lift and twist control using trailing edge control surfaces on supersonic laminar flow wings
AERION CORP18 citations82
US10296672B2May 21, 2019
Generating inviscid and viscous fluid-flow simulations over an aircraft surface using a fluid-flow mesh
AERION CORP5 citations81
US7967241B2Jun 28, 2011
Supersonic aircraft jet engine installation
AERION CORP12 citations80
US7000870B2Feb 21, 2006
Laminar flow wing for transonic cruise
AERION CORP8 citations72
US8935140B2Jan 13, 2015
Generating inviscid and viscous fluid-flow simulations over a surface using a fluid-flow mesh
AERION CORP4 citations70
US7946535B2May 24, 2011
Highly efficient supersonic laminar flow wing
AERION CORP4 citations61
US6857599B2Feb 22, 2005
Highly swept canard with low sweep wing supersonic aircraft configuration
AERION CORP6 citations61
US9348956B2May 24, 2016
Generating a simulated fluid flow over a surface using anisotropic diffusion
AERION CORP2 citations60
US8371124B2Feb 12, 2013
Jet nozzle plug with varying, non-circular cross sections
AERION CORP3 citations59
US11386245B2Jul 12, 2022
Computing techniques for three-dimensional modeling and design analysis
AERION CORP0 citations56
US9494482B2Nov 15, 2016
Predicting transition from laminar to turbulent flow over a surface using mode-shape parameters
AERION CORP0 citations49
US9418202B2Aug 16, 2016
Predicting transition from laminar to turbulent flow over a surface
AERION CORP0 citations49