Bücher zum Thema „Simulations rotor“
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Center, Ames Research, Hrsg. Three-dimensional Navier-Stokes simulations of turbine rotor-stator interaction. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.
Den vollen Inhalt der Quelle findenCenter, Ames Research, Hrsg. Three-dimensional Navier-Stokes simulations of turbine rotor-stator interaction. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.
Den vollen Inhalt der Quelle findenBoretti, A. A. Three-dimensional Euler time accurate simulations of fan rotor-stator interactions. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion, 1990.
Den vollen Inhalt der Quelle findenBoretti, A. A. Three-dimensional Euler time accurate simulations of fan rotor-stator interactions. Cleveland, Ohio: Lewis Research Centre, 1990.
Den vollen Inhalt der Quelle findenLewis Research Center. Institute for Computational Mechanics in Propulsion., Hrsg. Three-dimensional Euler time accurate simulations of fan rotor-stator interactions. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion, 1990.
Den vollen Inhalt der Quelle findenBoretti, A. A. Three-dimensional Euler time accurate simulations of fan rotor-stator interactions. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion, 1990.
Den vollen Inhalt der Quelle findenBoretti, A. A. Two-dimensional Euler and Navier Stokes time accurate simulations of fan rotor flows. Cleveland, Ohio: NASA Lewis Research Center, Institute for Computational Mechanics in Propulsion, 1990.
Den vollen Inhalt der Quelle findenBoretti, A. A. Two-dimensional Euler and Navier Stokes time accurate simulations of fan rotor flows. Cleveland, Ohio: NASA Lewis Research Center, Institute for Computational Mechanics in Propulsion, 1990.
Den vollen Inhalt der Quelle finden1950-, Hill Gary, und Ames Research Center, Hrsg. Comparisons of elastic and rigid blade-element rotor models using parallel processing technology for piloted simulations. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1991.
Den vollen Inhalt der Quelle findenP, Friedmann Peretz, und Ames Research Center, Hrsg. Aeroelastic simulation of higher harmonic control. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1994.
Den vollen Inhalt der Quelle findenPeretz, Friedmann, und Ames Research Center, Hrsg. Aeroelastic simulation of higher harmonic control. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1994.
Den vollen Inhalt der Quelle findenKen, Duisenberg, und Ames Research Center, Hrsg. Simulation of rotor blade element turbulence. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1995.
Den vollen Inhalt der Quelle findenChen, C. L. Numerical simulation of helicopter multi-bladed rotor flow. [New York]: American Institute of Aeronautics and Astronautics, 1988.
Den vollen Inhalt der Quelle findenCenter, Ames Research, Hrsg. Symbolic generation of elastic rotor blade equations using a FORTRAN processor and numerical study on dynamic inflow effects on the stability of helicopter rotors. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.
Den vollen Inhalt der Quelle findenE, Paxson D., Schobeiri M. T und United States. National Aeronautics and Space Administration., Hrsg. Dynamic simulation of a wave rotor topped turboshaft engine. [Washington, DC]: National Aeronautics and Space Administration, 1997.
Den vollen Inhalt der Quelle findenSopanen, Jussi. Studies of rotor dynamics using a multibody simulation approach. Lappeenranta: Lappeenranta University of Technology, 2004.
Den vollen Inhalt der Quelle findenR, Srinivasan G., Ames Research Center und United States. Army Aviation Research and Technology Activity., Hrsg. Flowfield of a lifting hovering rotor--a Navier-Stokes simulation. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., Hrsg. Performance of an optimized rotor blade at off-design flight conditions. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Den vollen Inhalt der Quelle findenChattopadhyay, Aditi. Performance of an optimized rotor blade at off-design flight conditions. Washington, DC: National Aeronautics and Space Administration, 1990.
Den vollen Inhalt der Quelle findenNovinschi, Anca. Simulation and implementation of rotor flux control for an induction motor. Leicester: De Montfort University, 1998.
Den vollen Inhalt der Quelle findenHamade, Karen S. Modal analysis of UH-60A instrumented rotor blades. Moffett Field, Calif: Ames Research Center, 1990.
Den vollen Inhalt der Quelle findenHamade, Karen S. Modal analysis of UH-60A instrumented rotor blades. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Den vollen Inhalt der Quelle findenM, Kufeld Robert, Ames Research Center und United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., Hrsg. Modal analysis of UH-60A instrumented rotor blades. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Den vollen Inhalt der Quelle findenM, Kufeld Robert, Ames Research Center und United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., Hrsg. Modal analysis of UH-60A instrumented rotor blades. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Den vollen Inhalt der Quelle findenRobinson, Christopher S. Modeling and analysis of helicopter ground resonance utilizing symbolic processing and dynamic simulation software. Monterey, Calif: Naval Postgraduate School, 1997.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., Hrsg. Three-dimensional numerical simulation of gradual opening in a wave rotor passage. [Washington, DC]: National Aeronautics and Space Administration, 1993.
Den vollen Inhalt der Quelle findenJ, Hall Edward, Delaney Robert A und Lewis Research Center, Hrsg. Follow-on low noise fan aerodynamic study: Task 15-final report. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1999.
Den vollen Inhalt der Quelle findenJ, Hall Edward, Delaney R. A und Lewis Research Center, Hrsg. Follow-on low noise fan aerodynamic study: Task 15-final report. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1999.
Den vollen Inhalt der Quelle findenJ, Hall Edward, Delaney Robert A und Lewis Research Center, Hrsg. Follow-on low noise fan aerodynamic study: Task 15-final report. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1999.
Den vollen Inhalt der Quelle findenKelly, Carney, Gallardo Vicente und NASA Glenn Research Center, Hrsg. Simulation of aircraft engine blade-out structural dynamics. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.
Den vollen Inhalt der Quelle findenKelly, Carney, Gallardo V. C und NASA Glenn Research Center, Hrsg. Simulation of aircraft engine blade-out structural dynamics. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., Hrsg. Prediction of helicopter rotor discrete frequency noise: A computer program incorporating realistic blade motions and advanced acoustic formulation. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
Den vollen Inhalt der Quelle findenMartinez, Debbie. The transition of a real-time single-rotor helicopter simulation program to a supercomputer. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Den vollen Inhalt der Quelle findenChaffin, Mark S. A guide to the use of the pressure disk rotor model as implemented in INS3D-UP. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Den vollen Inhalt der Quelle findenḤayimovits, Menaḥem. Model roṭor meshupar ṿe-shimusho le-simulatsyah shel masoḳ ḳerav mitḳadem. Ḥefah: ha-Merkaz le-meḥḳar aṿironoṭi, ha-Faḳulṭah le-handasah aṿironoṭit ṿe-ḥalal, ha-Tekhniyon, 1991.
Den vollen Inhalt der Quelle findenZomaya, Albert Y. A parallel Newton-Euler formulation for fast dynamic simulation of robor manipulators. Sheffield: University of Sheffield, Dept. of Control Engineering, 1989.
Den vollen Inhalt der Quelle findenVeletas, Mihalis. Integration of turbulence and ship wake disturbance models in the GENHEL-Sea King rotor simulation code. [Toronto]: University of Toronto Institute for Aerospace Studies, 1996.
Den vollen Inhalt der Quelle findenVeletas, Mihalis. Integration of turbulence and ship wake disturbance models in the GENHEL-Sea King rotor simulation code. Ottawa: National Library of Canada, 1996.
Den vollen Inhalt der Quelle findenC, Hendricks Robert, Steinetz Bruce M und United States. National Aeronautics and Space Administration., Hrsg. Numerical simulation of flow in a whirling annular seal and comparison with experiments. [Washington, DC]: National Aeronautics and Space Administration, 1995.
Den vollen Inhalt der Quelle findenKelly, Carney, Gallardo V. C und NASA Glenn Research Center, Hrsg. A study of fan stage/casing interaction models. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2003.
Den vollen Inhalt der Quelle findenCenter, Langley Research, Hrsg. Advanced turboprop aircraft flyover noise: Annoyance to counter-rotating-propeller configurations with a different number of blades on each rotor : preliminary results. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Den vollen Inhalt der Quelle findenCenter, Langley Research, Hrsg. Advanced turboprop aircraft flyover noise: Annoyance to counter-rotating-propeller configurations with an equal number of blades on each rotor : preliminary results. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Den vollen Inhalt der Quelle findenV, Nagpal, Chamis C. C und United States. National Aeronautics and Space Administration., Hrsg. Probabilistic analysis of bladed turbine disks and the effect of mistuning. [Washington, D.C: National Aeronautics and Space Administration, 1990.
Den vollen Inhalt der Quelle findenP, van Dam Cornelis, Duque Earl P. N und United States. National Aeronautics and Space Administration., Hrsg. Numerical simulation of helicopter engine plume in forward flight: Final report cooperative agreement #NCC2-5061. [Washington, DC: National Aeronautics and Space Administration, 1994.
Den vollen Inhalt der Quelle findenP, Van Dam C., Duque Earl P. N und United States. National Aeronautics and Space Administration., Hrsg. Numerical simulation of helicopter engine plume in forward flight: Final report cooperative agreement #NCC2-5061. [Washington, DC: National Aeronautics and Space Administration, 1994.
Den vollen Inhalt der Quelle findenK, Remple Robert, Hrsg. Aircraft and rotorcraft system identification: Engineering methods with flight test examples. 2. Aufl. Reston, VA: American Institute of Aeronautics and Astronautics, 2012.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., Hrsg. Application of a two-dimensional unsteady viscous analysis code to a supersonic throughflow fan stage. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Den vollen Inhalt der Quelle findenSteinke, Ronald J. Application of a two-dimensional unsteady viscous analysis code to a supersonic throughflow fan stage. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., Hrsg. Application of a two-dimensional unsteady viscous analysis code to a supersonic throughflow fan stage. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Den vollen Inhalt der Quelle findenSteinke, Ronald J. Application of a two-dimensional unsteady viscous analysis code to a supersonic throughflow fan stage. Cleveland, Ohio: Lewis Research Center, 1989.
Den vollen Inhalt der Quelle finden