Książki na temat „Simulations rotor”

Center, Ames Research, red. Three-dimensional Navier-Stokes simulations of turbine rotor-stator interaction. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

Center, Ames Research, red. Three-dimensional Navier-Stokes simulations of turbine rotor-stator interaction. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

Boretti, 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.

Boretti, A. A. Three-dimensional Euler time accurate simulations of fan rotor-stator interactions. Cleveland, Ohio: Lewis Research Centre, 1990.

Lewis Research Center. Institute for Computational Mechanics in Propulsion., red. 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.

Boretti, 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.

Boretti, 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.

Boretti, 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.

1950-, Hill Gary, i Ames Research Center, red. 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.

P, Friedmann Peretz, i Ames Research Center, red. Aeroelastic simulation of higher harmonic control. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1994.

Peretz, Friedmann, i Ames Research Center, red. Aeroelastic simulation of higher harmonic control. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1994.

Ken, Duisenberg, i Ames Research Center, red. Simulation of rotor blade element turbulence. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1995.

Chen, C. L. Numerical simulation of helicopter multi-bladed rotor flow. [New York]: American Institute of Aeronautics and Astronautics, 1988.

Center, Ames Research, red. 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.

E, Paxson D., Schobeiri M. T i United States. National Aeronautics and Space Administration., red. Dynamic simulation of a wave rotor topped turboshaft engine. [Washington, DC]: National Aeronautics and Space Administration, 1997.

Sopanen, Jussi. Studies of rotor dynamics using a multibody simulation approach. Lappeenranta: Lappeenranta University of Technology, 2004.

R, Srinivasan G., Ames Research Center i United States. Army Aviation Research and Technology Activity., red. Flowfield of a lifting hovering rotor--a Navier-Stokes simulation. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., red. 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.

Chattopadhyay, Aditi. Performance of an optimized rotor blade at off-design flight conditions. Washington, DC: National Aeronautics and Space Administration, 1990.

Novinschi, Anca. Simulation and implementation of rotor flux control for an induction motor. Leicester: De Montfort University, 1998.

Hamade, Karen S. Modal analysis of UH-60A instrumented rotor blades. Moffett Field, Calif: Ames Research Center, 1990.

Hamade, 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.

M, Kufeld Robert, Ames Research Center i United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., red. 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.

M, Kufeld Robert, Ames Research Center i United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., red. 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.

Robinson, Christopher S. Modeling and analysis of helicopter ground resonance utilizing symbolic processing and dynamic simulation software. Monterey, Calif: Naval Postgraduate School, 1997.

United States. National Aeronautics and Space Administration., red. Three-dimensional numerical simulation of gradual opening in a wave rotor passage. [Washington, DC]: National Aeronautics and Space Administration, 1993.

J, Hall Edward, Delaney Robert A i Lewis Research Center, red. Follow-on low noise fan aerodynamic study: Task 15-final report. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1999.

J, Hall Edward, Delaney R. A i Lewis Research Center, red. Follow-on low noise fan aerodynamic study: Task 15-final report. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1999.

J, Hall Edward, Delaney Robert A i Lewis Research Center, red. Follow-on low noise fan aerodynamic study: Task 15-final report. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1999.

Kelly, Carney, Gallardo Vicente i NASA Glenn Research Center, red. Simulation of aircraft engine blade-out structural dynamics. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

Kelly, Carney, Gallardo V. C i NASA Glenn Research Center, red. Simulation of aircraft engine blade-out structural dynamics. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., red. 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.

Martinez, 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.

Chaffin, 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.

Ḥayimovits, 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.

Zomaya, Albert Y. A parallel Newton-Euler formulation for fast dynamic simulation of robor manipulators. Sheffield: University of Sheffield, Dept. of Control Engineering, 1989.

Veletas, 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.

Veletas, Mihalis. Integration of turbulence and ship wake disturbance models in the GENHEL-Sea King rotor simulation code. Ottawa: National Library of Canada, 1996.

C, Hendricks Robert, Steinetz Bruce M i United States. National Aeronautics and Space Administration., red. Numerical simulation of flow in a whirling annular seal and comparison with experiments. [Washington, DC]: National Aeronautics and Space Administration, 1995.

Kelly, Carney, Gallardo V. C i NASA Glenn Research Center, red. A study of fan stage/casing interaction models. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2003.

Center, Langley Research, red. 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.

Center, Langley Research, red. 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.

V, Nagpal, Chamis C. C i United States. National Aeronautics and Space Administration., red. Probabilistic analysis of bladed turbine disks and the effect of mistuning. [Washington, D.C: National Aeronautics and Space Administration, 1990.

P, van Dam Cornelis, Duque Earl P. N i United States. National Aeronautics and Space Administration., red. Numerical simulation of helicopter engine plume in forward flight: Final report cooperative agreement #NCC2-5061. [Washington, DC: National Aeronautics and Space Administration, 1994.

P, Van Dam C., Duque Earl P. N i United States. National Aeronautics and Space Administration., red. Numerical simulation of helicopter engine plume in forward flight: Final report cooperative agreement #NCC2-5061. [Washington, DC: National Aeronautics and Space Administration, 1994.

K, Remple Robert, red. Aircraft and rotorcraft system identification: Engineering methods with flight test examples. Wyd. 2. Reston, VA: American Institute of Aeronautics and Astronautics, 2012.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., red. 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.

Steinke, 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.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., red. 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.

Steinke, Ronald J. Application of a two-dimensional unsteady viscous analysis code to a supersonic throughflow fan stage. Cleveland, Ohio: Lewis Research Center, 1989.