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非定常運動翼による高揚力・高推進力発生機構の解明とその効果的応用

非定常運動翼による高揚力・高推進力発生機構の解明とその効果的応用
Paper図書
田中和博, 九州工業大学 [著][田中和博]2003-2005<Y151-H15360098>
National Diet Library

Dynamic behavior of separation vortices around a pitching and heaving airfoils and dynamic forces : ヒ-ビング・ピツチング運動翼まわりの非 定常はく離渦の挙動とその流体力への影響

Dynamic behavior of separation vortices around a pitching and heaving airfoils and dynamic forces : ヒ-ビング・ピツチング運動翼まわりの非 定常はく離渦の挙動とその流体力への影響
Paper図書
田中, 和博, 九州工業大学2001-2002<Y151-H13650187>
National Diet Library

An experimental and computational investigation of oscillating airfoil unsteady aerodynamics at large mean incidence [microform] / Vincent R. Capece, Max F. Platzer (NASA/CR-2003-212199)

An experimental and computational investigation of oscillating airfoil unsteady aerodynamics at large mean incidence [microform] / Vincent R. Capece, Max F. Platzer (NASA/CR-2003-212199)
Microform図書
2003<YCA-NAS 1.26:212199>
National Diet Library
  • Subject Heading...Turbomachinery Airfoils Aeroelasticity Gas turbine en...

Experimental investigation of water droplet impingement on airfoils, finite wings, and an S-duct engine inlet [microform] / Michael Papadakis ... [et al.] (NASA/TM-2002-211700)

Experimental investigation of water droplet impingement on airfoils, finite wings, and an S-duct engine inlet [microform] / Michael Papadakis ... [et al.] (NASA/TM-2002-211700)
Microform図書
2002<YCA-NAS 1.15:2002-211700>
National Diet Library
  • Subject HeadingWater Drops (Liquids) Impingement Airfoils Wings Engine inlets

Computer program to obtain ordinates for NACA airfoils [microform] / Charles L. Ladson ... [et al.] (NASA technical memorandum ; 4741)

Computer program to obtain ordinates for NACA airfoils [microform] / Charles L. Ladson ... [et al.] (NASA technical memorandum ; 4741)
Microform図書
1996<YCA-NAS 1.15:4741>
National Diet Library
  • Subject HeadingComputer programs Airfoil profiles Airfoils

Transient growth theory prediction of optimal placing of passive and active flow control devices for separation delay in LPT airfoils [microform] / Anatoli Tumin, David E. Ashpis ([NASA technical memorandum] ; NASA/TM-2003-212228)

Transient growth theory prediction of optimal placing of passive and active flow control devices for separation delay in LPT airfoils [microform] / Anatoli Tumin, David E. Ashpis ([NASA technical memorandum] ; NASA/TM-2003-212228)
Microform図書
National Aeronautics and Space Administration, Glenn Research Center[2003]<YCA-NAS 1.15:212228>
National Diet Library
  • Subject HeadingAirfoils Control equipment Flow stabil...

Free-form airfoil shape optimization under uncertainty using maximum expected value and second-order second-moment strategies [microform] / Luc Huyse (ICASE report ; no. 2001-18) ([NASA contractor report] ; NASA/CR-2001-211020)

Free-form airfoil shape optimization under uncertainty using maximum expected value and second-order second-moment strategies [microform] / Luc Huyse (ICASE report ; no. 2001-18) ([NASA contractor report] ; NASA/CR-2001-211020)
Microform図書
2001<YCA-NAS 1.26:211020>
National Diet Library
  • Subject HeadingAirfoils Shape optimization Statistica...

Aerodynamic shape optimization of two-dimensional airfoils under uncertain conditions [microform] / Luc Huyse, R. Michael Lewis (ICASE report ; no. 2001-1) ([NASA contractor report] ; NASA/CR-2001-210648)

Aerodynamic shape optimization of two-dimensional airfoils under uncertain conditions [microform] / Luc Huyse, R. Michael Lewis (ICASE report ; no. 2001-1) ([NASA contractor report] ; NASA/CR-2001-210648)
Microform図書
2001<YCA-NAS 1.26:210648>
National Diet Library
  • Subject HeadingAirfoils Optimization Aerodynamic conf...
  • Alternative TitleAerodynamic shape optimization of two dimensional airfoils under uncertain conditions
  • Alternative TitleAerodynamic shape optimization of two dimensional airfoils under uncertain conditions

Unsteady cascade aerodynamic response using a multiphysics simulation code [microform] / C. Lawrence, E. Spyropoulos, T.S.R. Reddy (NASA/TM ; 2000-209635)

Unsteady cascade aerodynamic response using a multiphysics simulation code [microform] / C. Lawrence, E. Spyropoulos, T.S.R. Reddy (NASA/TM ; 2000-209635)
Microform図書
2000<YCA-NAS 1.15:209635>
National Diet Library
  • Subject Heading...haracteristics Airfoils Computerized simulation

Optimization with variable-fidelity models applied to wing design [microform] / Natalia M. Alexandrov ... [et al.] (ICASE report ; no. 99-49) ([NASA contractor report] ; NASA/CR-1999-209826)

Optimization with variable-fidelity models applied to wing design [microform] / Natalia M. Alexandrov ... [et al.] (ICASE report ; no. 99-49) ([NASA contractor report] ; NASA/CR-1999-209826)
Microform図書
1999<YCA-NAS 1.26:209826>
National Diet Library
  • Subject HeadingAlgorithms Nonlinear programming Design analysis Wings Airfoils

Ice accretions and icing effects for modern airfoils [microform] / Harold E. Addy, Jr (NASA/TP ; 2000-210031)

Ice accretions and icing effects for modern airfoils [microform] / Harold E. Addy, Jr (NASA/TP ; 2000-210031)
Microform図書
2000<YCA-NAS 1.60:210031>
National Diet Library
  • Subject HeadingDeposition Ice Aircraft icing Two dimensional bodies Airfoils Aerodynamic characteristics

SiC/SiC leading edge turbine airfoil tested under simulated gas turbine conditions [microform] / R. Craig Robinson, Kenneth S. Hatton ([NASA contractor report] ; NASA/CR-1999-209314)

SiC/SiC leading edge turbine airfoil tested under simulated gas turbine conditions [microform] / R. Craig Robinson, Kenneth S. Hatton ([NASA contractor report] ; NASA/CR-1999-209314)
Microform図書
1999<YCA-NAS 1.26:209314>
National Diet Library
  • Subject HeadingSilicon Leading edges Airfoils Gas turbine engines Design an...

Airfoil dynamic stall and rotorcraft maneuverability [microform] / William G. Bousman ([NASA technical memorandum] ; NASA/TM-2000-209601)

Airfoil dynamic stall and rotorcraft maneuverability [microform] / William G. Bousman ([NASA technical memorandum] ; NASA/TM-2000-209601)
Microform図書
2000<YCA-NAS 1.15:209601>
National Diet Library

Continued development and application of circulation control pneumatic technology to advanced transport aircraft [microform] : NASA grant NAG-1-1517 : period covered, June 14, 1993 to August 31, 1997 / by Robert J. Englar, principal investigator ([NASA contractor report] ; NASA/CR-207471)

Continued development and application of circulation control pneumatic technology to advanced transport aircraft [microform] : NASA grant NAG-1-1517 : period covered, June 14, 1993 to August 31, 1997 / by Robert J. Englar, principal investigator ([NASA contractor report] ; NASA/CR-207471)
Microform図書
1998<YCA-NAS 1.26:207471>
National Diet Library
  • Subject HeadingTechnologies Aerodynamics Pneumatics Airfoils Dynamic control Transport air...

The effects of the critical ice accretion on airfoil and wing performance [microform] : NASA contract # NCC3-408 : January 24, 1995-November 30, 1996 : final report / Michael S. Selig, Michael B. Bragg, and Farooq Saeed ([NASA contractor report] ; NASA/CR 207501)

The effects of the critical ice accretion on airfoil and wing performance [microform] : NASA contract # NCC3-408 : January 24, 1995-November 30, 1996 : final report / Michael S. Selig, Michael B. Bragg, and Farooq Saeed ([NASA contractor report] ; NASA/CR 207501)
Microform図書
1998<YCA-NAS 1.26:207501>
National Diet Library
  • Subject HeadingAerodynamic characteristics Design analysis Airfoils Leading edges Ice formation

Effects of suction on swept-wing transition [microform] : final technical report on NASA-Langley award # NAG-1-194, 16 December 1995 to 31 March 1998 / by William S. Saric ([NASA contractor report] ; 206838)

Effects of suction on swept-wing transition [microform] : final technical report on NASA-Langley award # NAG-1-194, 16 December 1995 to 31 March 1998 / by William S. Saric ([NASA contractor report] ; 206838)
Microform図書
1998<YCA-NAS 1.26:206838>
National Diet Library
  • Subject HeadingExperimentation Swept wings Suction Surface defects Cross flow Airfoils

Numerical study of turbulence model predictions for the MD 30P/30N and NHLP-2D three-element highlift configurations [microform] / Joseph H. Morrison ([NASA contractor report] ; NASA/CR-1998-208967)

Numerical study of turbulence model predictions for the MD 30P/30N and NHLP-2D three-element highlift configurations [microform] / Joseph H. Morrison ([NASA contractor report] ; NASA/CR-1998-208967)
Microform図書
1998<YCA-NAS 1.26:208967>
National Diet Library
  • Subject HeadingTurbulence models Airfoils Reynolds averaging Navier-Sto...

TADS--a CFD-based turbomachinery analysis and design system with GUI [microform] : version 2.0--methods and results / M.J. Koiro, R.A. Myers, and R.A. Delaney ([NASA contractor report] ; NASA/CR-1999-206603)

TADS--a CFD-based turbomachinery analysis and design system with GUI [microform] : version 2.0--methods and results / M.J. Koiro, R.A. Myers, and R.A. Delaney ([NASA contractor report] ; NASA/CR-1999-206603)
Microform図書
1999<YCA-NAS 1.26:206603>
National Diet Library
  • Subject Heading...stems analysis Airfoils Design analysis

Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program [microform] / Bruce Charles ([NASA contractor report] ; NASA/CR-1999-209327)

Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program [microform] / Bruce Charles ([NASA contractor report] ; NASA/CR-1999-209327)
Microform図書
1999<YCA-NAS 1.26:209327>
National Diet Library
  • Subject Heading...oise pollution Airfoils

A preconditioning method for shape optimization governed by the Euler equations [microform] / Eyal Arian, Veer N. Vatsa (ICASE report ; no. 98-14) ([NASA contractor report] ; NASA/CR-1998-206926)

A preconditioning method for shape optimization governed by the Euler equations [microform] / Eyal Arian, Veer N. Vatsa (ICASE report ; no. 98-14) ([NASA contractor report] ; NASA/CR-1998-206926)
Microform図書
1998<YCA-NAS 1.26:206926>
National Diet Library
  • Subject Heading...pressible flow Airfoils Computational fluid dynamics ...