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A study of three dimensional turbulent boundary layer separation and vortex flow control using the reduced Navier Stokes equations [microform] / Bernhard H. Anderson and Saeed Farokhi.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]
1991
0 resources
Application of computational fluid dynamics to the study of vortex flow control for the management of inlet distortion [microform] / Bernhard H. Anderson and James Gibb.
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1992]
1992
0 resources
A design strategy for the use of vortex generators to manage inlet-engine distortion using computational fluid dynamics [microform] / Bernhard H. Anderson and Ralph Levy.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
1991
0 resources
The aerodynamic characteristics of vortex ingestion for the F/A-18 inlet duct [microform] / Bernhard H. Anderson.
Text
[Washington, DC] : NASA ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
1991
0 resources
A robust design methodology for optimal microscale secondary flow control in compact inlet diffusers [microform] / Bernhard H. Anderson, Dennis J. Keller.
Text
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
2001
1 resource
Available online
Adobe Acrobat Reader requiredManagement of total pressure recovery, distortion and high cycle fatigue in compact air vehicle inlets [microform] / Bernhard H. Anderson, Henry D. Baust, Johan Agrell.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center ; Hanover MD : Available from NASA Center for AeroSpace Information, [2002]
2002
1 resource
Available online
Adobe Acrobat Reader requiredDesign-of-experiments to reduce life-cycle costs in combat aircraft inlets [microform] / Bernhard H. Anderson, Henry D. Baust, [and] Johan Agrell.
Text
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover MD : Available from NASA Center for AeroSpace Information, [2003]
2003
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS46082Three-dimensional viscous design methedology for advanced technology aircraft supersonic inlet systems [microform] / Bernhard H. Anderson.
Text
[Washington, D.C. : National Aeronautics and Space Administration, 1984]
1984
0 resources
Management of total pressure recovery, distortion and high cycle fatigue in compact air vehicle inlets / Bernhard H. Anderson, Henry D. Baust, Johan Agrell.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, December 2002.
2002-12
1 resource
Available online
https://purl.fdlp.gov/GPO/LPS36341Design-of-experiments to reduce life-cycle costs in combat aircraft inlets / Bernhard H. Anderson, Henry D. Baust, Johan Agrell.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, January 2003.
2003-1
1 resource
Available online
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