Crossref Citations
This article has been cited by the following publications. This list is generated based on data provided by
Crossref.
O’Brien, C. W.
Snyder, M. R.
Hallberg, E. N.
and
Cenko, A.
2012.
Effects of targeting pod modification on F/A-18C Hornet weapons release.
The Aeronautical Journal,
Vol. 116,
Issue. 1181,
p.
743.
Luckring, James M.
Park, Michael A.
Hitzel, Stephan M.
Jirásek, Adam
Lofthouse, Andrew J.
Morton, Scott A.
McDaniel, David R.
Rizzi, Arthur
and
Tomac, Maximillian
2017.
Synthesis of Hybrid Computational Fluid Dynamics Results for F-16XL Aircraft Aerodynamics.
Journal of Aircraft,
Vol. 54,
Issue. 6,
p.
2100.
Viken, Jeffrey K.
Viken, Sally
Deere, Karen A.
and
Carter, Melissa
2017.
Design of the Cruise and Flap Airfoil for the X-57 Maxwell Distributed Electric Propulsion Aircraft.
Powell, Nicholas A.
Clemens, Andrew
Velez-Valencia, Andres
and
Welter, Jack
2018.
Gulfstream's Contributions to the Third AIAA High Lift Prediction Workshop.
Winski, Courtney S.
Carter, Melissa B.
Elmiligui, Alaa A.
Pearl, Jason M.
Nayani, Sudheer N.
and
Durston, Donald A.
2018.
Computational and Experimental Study of Plume and Shock Interaction Effects on Sonic Boom in the NASA Ames 9x7 Supersonic Wind Tunnel.
Majewski, Jerzy
Szałtys, Piotr
and
Wyrozębski, Marcin
2018.
Residual distribution method for high Reynolds number simulations on complex geometries.
Computers & Fluids,
Vol. 166,
Issue. ,
p.
104.
Galbraith, Marshall C.
Allmaras, Steven R.
and
Darmofal, David L.
2018.
SANS RANS solutions for 3D benchmark configurations.
Green, Bradford E.
Czerwiec, Ryan
Shafer, Theresa C.
and
Rhinehart, Mackenzie
2018.
CFD Predictions of the Stability and Control Characteristics of the E-2D Advanced Hawkeye.
Deere, Karen A.
Viken, Sally
Carter, Melissa B.
Viken, Jeffrey K.
Cox, David E.
Wiese, Michael R.
and
Farr, Norma L.
2018.
Computational Component Build-up for the X-57 Maxwell Distributed Electric Propulsion Aircraft.
Cunningham, Kevin
Shah, Gautam H.
Frink, Neal T.
McMillin, Susan N.
Murphy, Patrick C.
Brown, Frank R.
Hayes, Patrick J.
Shweyk, Kamal M.
and
Nayani, Sudheer N.
2018.
Preliminary Test Results for Stability and Control Characteristics of a Generic T-tail Transport Airplane at High Angle of Attack.
van Rooij, Michel
Frink, Neal T.
Hiller, Brett R.
Ghoreyshi, Mehdi
and
Voskuijl, Mark
2018.
Generation of a Reduced Order Model of an Unmanned Combat Air Vehicle using Indicial Response Functions.
Eggert, Christopher A.
Shea, Patrick R.
Ratnayake, Nalin A.
and
Krist, Steven E.
2019.
Effect of Sting Geometry on Axial Force Calculation for the Space Launch System.
McMillin, Susan N.
Frink, Neal T.
Murphy, Patrick C.
Cunningham, Kevin
Shah, Gautam H.
and
Nayani, Sudheer N.
2019.
Computational Study of a Generic T-tail Transport.
Park, Michael A.
and
Nemec, Marian
2019.
Nearfield Summary and Statistical Analysis of the Second AIAA Sonic Boom Prediction Workshop.
Journal of Aircraft,
Vol. 56,
Issue. 3,
p.
851.
Elmiligui, Alaa
Carter, Melissa B.
Nayani, Sudheer N.
Cliff, Susan
and
Pearl, Jason M.
2019.
USM3D Simulations for Second Sonic Boom Workshop.
Journal of Aircraft,
Vol. 56,
Issue. 3,
p.
928.
Luckring, J.M.
2019.
The discovery and prediction of vortex flow aerodynamics.
The Aeronautical Journal,
Vol. 123,
Issue. 1264,
p.
729.
Frink, Neal T.
Hiller, Brett R.
Murphy, Patrick C.
Cunningham, Kevin
and
Shah, Gautam H.
2019.
Investigation of Reduced-Order Modeling for Aircraft Stability and Control Prediction.
Green, Bradford E.
and
Czerwiec, Ryan
2019.
CFD Analysis of the F/A-18E Super Hornet during Extension and Retraction of the Landing Gear.
Ratnayake, Nalin A.
Krist, Steven E.
Ghaffari, Farhad
and
Deere, Karen A.
2019.
Computational Fluid Dynamics Methods Used in the Development of the Space Launch System Liftoff and Transition Lineloads Databases.
van Rooij, Michel P.C.
Frink, Neal T.
Hiller, Brett R.
Ghoreyshi, Mehdi
and
Voskuijl, Mark
2019.
Generation of a reduced-order model of an Unmanned Combat Air Vehicle using indicial response functions.
Aerospace Science and Technology,
Vol. 95,
Issue. ,
p.
105510.