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1
Unsteady hybrid vortex technique for transonic vortex flows and flutter applications
Norfolk, Va. : Dept. of Mechanical Engineering and Mechanics, College of Engineering and Technology, Old Dominion University, 1987Format: Government Document Book
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2
Analysis and control of supersonic vortex breakdown flows
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1990Format: Government Document Book
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3
Unsteady hybrid vortex technique for transonic vortex flows and flutter applications
Norfolk, Va. : [Washington, DC : Springfield, Va. : Old Dominion University Research Foundation ; National Aeronautics and Space Administration ; National Technical Information Service, distributor, 1987Format: Government Document Book
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4
Aerostructural vortical flow interactions with applications to F/A-18 and F-117 tail buffet
[Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1996Format: Government Document Book
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5
Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications : final report for the period December 1, 1995 through November 30, 1996
Norfolk, Va. : [Washington, DC] : [Springfield, Va.] : Dept. of Aerospace Engineering, College of Engineering & Technology, Old Dominion University ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1997Format: Government Document Book
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6
Three dimensional solution of pneumatic active control of forebody vortex asymmetry
Washington, D.C. : [Springfield, Va.] : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1995Format: Government Document Book
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7
Analysis and control of supersonic vortex breakdown flows
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1990Format: Government Document Book
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8
Aeroelastic, CFD, and dynamic computation and optimization for buffet and flutter application : final report for the period of December 1, 1996-November 30, 1997 : under research g...
Norfolk, Va. : [Washington, DC] : [Springfield, Va.] : Dept. of Aerospace Engineering, College of Engineering and Technology, Old Dominion University ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1997Format: Government Document Book
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9
Unsteady hybrid vortex technique for transonic vortex flows and flutter applications
Norfolk, Va. : [Washington, DC] : [Springfield, Va.] : Old Dominion University Research Foundation ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1987Format: Government Document Book
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10
Twin tail/Delta wing configuration buffet due to unsteady vortex breakdown flow
[Washington, D.C.] : [National Aeronautics and Space Administration], 1997Format: Government Document Book
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11
Computation technique for compressible vortex flows using the integral equation solution : final report
Norfolk, Va. : Dept. of Mechanical Engineering and Mechanics, College of Engineering, Old Dominion University, 1988Format: Government Document Book
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12
Computation technique for compressible vortex flows using the integral equation solution final report
Norfolk, Va. : Dept. of Mechanical Engineering and Mechanics, College of Engineering, Old Dominion University, 1988Format: Government Document Book
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13
Effective control of computationally simulated wing rock in subsonic flow
[Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1997Format: Government Document Book
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14
Navier-Stokes dynamics and aeroelastic computations for vortical flows, buffet and aeroelastic applications
Norfolk, Va. : [Washington, DC] : [Springfield, Va.] : Old Dominion University Research Foundation ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1992Format: Government Document Book
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15
Analysis and control of asymmetric vortex flows and supersonic vortex breakdown : final report for the period December 1, 1991 to November 30, 1992
Norfolk, Va. : [Washington, D.C.] : [Springfield, Va.] : Old Dominion University Research Foundation ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1992Format: Government Document Book
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16
Far-field turbulent vortex-wake/exhaust plume interaction for subsonic and HSCT airplanes : 27th AIAA Fluid Dynamics Conference, June 17-20, 1996/New Orleans, LA
Washington, DC : [Springfield, Va.] : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1996Format: Government Document Book
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17
Analysis and control of asymmetric vortex flows and supersonic vortex breakdown
Norfolk, Va. : Hampton, Va. : Dept. of Mechanical Engineering & Mechanics, College of Engineering & Technology, Old Dominion University ; National Aeronautics and Space Administration, Langley Research Center, 1991Format: Government Document Book
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18
Development of disturbances in swept wing flows : final report
Norfolk, Va. : Dept. of Mechanical Engineering and Mechanics, College of Engineering and Technology, Old Dominion University, 1988Format: Government Document Book
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19
Development of disturbances in swept wing flows final report
Norfolk, Va. : Dept. of Mechanical Engineering and Mechanics, College of Engineering and Technology, Old Dominion University, 1988Format: Government Document Book
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20
Computation and validation of fluid/structure twin tail buffet response
[Washington, D.C.] : [National Aeronautics and Space Administration], 1997Format: Government Document Conference Proceeding Book