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Search results 19

NASA space transportation architecture study at very high angles of attack AIAA-2001-0703

NASA space transportation architecture study at very high angles of attack AIAA-2001-0703
Paper規格・テクニカルリポート類
Kandil, Osama A, Yang, Zhi, Pelaez, Juan A, Mavriplis, Dimitri2001<M-AIAA-2001-0703>
National Diet Library

Development and application of adaptive dynamic grid for wake-vortex/ground interaction AIAA-2000-0789

Development and application of adaptive dynamic grid for wake-vortex/ground interaction AIAA-2000-0789
Paper規格・テクニカルリポート類
Turkgeldi, Ilker E, Kandil, Osama A2000<M-AIAA-2000-0789>
National Diet Library

Effect of dynamic rolling oscillations on twin tail buffet response AIAA-99-0792

Effect of dynamic rolling oscillations on twin tail buffet response AIAA-99-0792
Paper規格・テクニカルリポート類
Sheta, Essam F, Kandil, Osama A1999<M-AIAA-99-0792>
National Diet Library

Effect of reduced frequency on super maneuver delta wing AIAA-98-0415

Effect of reduced frequency on super maneuver delta wing AIAA-98-0415
Paper規格・テクニカルリポート類
Abdelhamid, Yahia A, Kandil, Osama A1998<M-AIAA-98-0415>
National Diet Library

Effect of configuration pitching motion on twin tail buffet response AIAA-98-0520

Effect of configuration pitching motion on twin tail buffet response AIAA-98-0520
Paper規格・テクニカルリポート類
Sheta, Essam F, Kandil, Osama A1998<M-AIAA-98-0520>
National Diet Library

Flow control and modification for alleviating twin-tail buffet AIAA-99-0138

Flow control and modification for alleviating twin-tail buffet AIAA-99-0138
Paper規格・テクニカルリポート類
Kandil, Osama A, Yang, Zhi, Sheta, Essam F1999<M-AIAA-99-0138>
National Diet Library

Investigation of three-dimensional vortex-wake interaction with the ground AIAA-98-0594

Investigation of three-dimensional vortex-wake interaction with the ground AIAA-98-0594
Paper規格・テクニカルリポート類
Adam, Ihab G, Kandil, Osama A1998<M-AIAA-98-0594>
National Diet Library

Effectiveness of flow control for alleviation of twin-tail buffet SAE-985501

Effectiveness of flow control for alleviation of twin-tail buffet SAE-985501
Paper規格・テクニカルリポート類
Shetta, Essam F, Kandil, Osama A, Yang, Zhi1998<M-SAE-985501>
National Diet Library

Effective control of computationally simulated wing rock in subsonic flow AIAA-97-0831

Effective control of computationally simulated wing rock in subsonic flow AIAA-97-0831
Paper規格・テクニカルリポート類
Kandil, Osama A, Menzies, Margaret A1997<M-AIAA-97-0831>
National Diet Library

Effective control of computationally simulated wing rock in subsonic flow [microform] / Osama A. Kandil and Margaret A. Menzies

Effective control of computationally simulated wing rock in subsonic flow [microform] / Osama A. Kandil and Margaret A. Menzies
Microform図書
1997<YCA-NAS 1.26:203247>
National Diet Library
  • Author HeadingKandil, Osama A United States. National Aeron...

Coupled rolling and pitching oscillation effects on transonic shock-induced vortex-breakdown flow of a delta wing AIAA-96-0828

Coupled rolling and pitching oscillation effects on transonic shock-induced vortex-breakdown flow of a delta wing AIAA-96-0828
Paper規格・テクニカルリポート類
Kandil, Osama A, Menzies, Margaret A1996<M-AIAA-96-0828>
National Diet Library

Twin tail/Delta wing configuration buffet due to unsteady vortex breakdown flow [microform] / Osama A. Kandil, Essam F. Sheta, and Steven J. Massey ([NASA contractor report] ; NASA-CR-203258)

Twin tail/Delta wing configuration buffet due to unsteady vortex breakdown flow [microform] / Osama A. Kandil, Essam F. Sheta, and Steven J. Massey ([NASA contractor report] ; NASA-CR-203258)
Microform図書
1997<YCA-NAS 1.26:203258>
National Diet Library
  • Author HeadingKandil, Osama A Sheta, Essam F Massey, Steven...

Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications [microform] : final report for the period December 1, 1995 through Novemeber 30, 1996 / principal investigator, Osama A. Kandil ; submitted by the Old Dominion University Research Foundation ([NASA contractor report] ; NASA-CR-203244)

Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications [microform] : final report for the period December 1, 1995 through Novemeber 30, 1996 / principal investigator, Osama A. Kandil ; submitted by the Old Dominion University Research Foundation ([NASA contractor report] ; NASA-CR-203244)
Microform図書
1997<YCA-NAS 1.26:203244>
National Diet Library
  • Author HeadingKandil, Osama A Old Dominion University. Rese...

Aeroelastic, CFD, and dynamic computation and optimization for buffet and flutter application [microform] : final report for the period of December 1, 1996-November 30, 1997 : under research grant NAG-1-648 / by Osama A. Kandil, principal investigator ; submitted by Old Dominion University Research Foundation ([NASA contractor report] ; 206678)

Aeroelastic, CFD, and dynamic computation and optimization for buffet and flutter application [microform] : final report for the period of December 1, 1996-November 30, 1997 : under research grant NAG-1-648 / by Osama A. Kandil, principal investigator ; submitted by Old Dominion University Research Foundation ([NASA contractor report] ; 206678)
Microform図書
1997<YCA-NAS 1.26:206678>
National Diet Library
  • Author HeadingKandil, Osama A Old Dominion University. Rese...

Aerostructural vortical flow interactions with applications to F/A-18 and F-117 tail buffet [microform] / Osama A. Kandil, Steven J. Massey and Essam F. Sheta ([NASA contractor report] ; NASA-CR-203245)

Aerostructural vortical flow interactions with applications to F/A-18 and F-117 tail buffet [microform] / Osama A. Kandil, Steven J. Massey and Essam F. Sheta ([NASA contractor report] ; NASA-CR-203245)
Microform図書
1996<YCA-NAS 1.26:203245>
National Diet Library
  • Author HeadingKandil, Osama A Massey, Steven J Sheta, Essam...

Computation and validation of fluid/structure twin tail buffet response [microform] / [Osama A. Kandil and Essam F. Sheta, C.H. Liu] ([NASA contractor report] ; NASA-CR-203259)

Computation and validation of fluid/structure twin tail buffet response [microform] / [Osama A. Kandil and Essam F. Sheta, C.H. Liu] ([NASA contractor report] ; NASA-CR-203259)
Microform図書
1997<YCA-NAS 1.26:203259>
National Diet Library
  • Author HeadingKandil, Osama A Sheta, Essam F Liu, C. H. (Ch...

Far-field turbulent vortex-wake/exhaust plume interaction for subsonic and HSCT airplanes [microform] : 27th AIAA Fluid Dynamics Conference, June 17-20, 1996/New Orleans, LA / Osama A. Kandil, Ihab Adam and Tin-Chee Wong ([NASA contractor report] ; NASA-CR-203260)

Far-field turbulent vortex-wake/exhaust plume interaction for subsonic and HSCT airplanes [microform] : 27th AIAA Fluid Dynamics Conference, June 17-20, 1996/New Orleans, LA / Osama A. Kandil, Ihab Adam and Tin-Chee Wong ([NASA contractor report] ; NASA-CR-203260)
Microform図書
1996<YCA-NAS 1.26:203260>
National Diet Library
  • Author HeadingKandil, Osama A Adam, Ihab Wong, Tin-Chee Ame...

EFFECTIVE CONTROL OF COMPUTATIONALLY SIMULATED WING ROCK IN SUBSONIC FLOW (NASA ; NASA-CR-213247)

EFFECTIVE CONTROL OF COMPUTATIONALLY SIMULATED WING ROCK IN SUBSONIC FLOW (NASA ; NASA-CR-213247)
Paper図書
KANDIL,OSAMA A. (OLD DOMINION UNIV.)National Aeronautics and Space Administration(National Aeronautics and Space Administration)1997.
Other Libraries in Japan

Three dimensional solution of pneumatic active control of forebody vortex asymmetry AIAA-95-0101

Three dimensional solution of pneumatic active control of forebody vortex asymmetry AIAA-95-0101
Paper規格・テクニカルリポート類
Kandil, Osama A, El-Din, Hazem H. Sharaff, Liu, C. H<M-AIAA-95-0101>
National Diet Library

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