3 edition of **Unsteady blade-surface pressures on a large-scale advanced propeller** found in the catalog.

Unsteady blade-surface pressures on a large-scale advanced propeller

- 397 Want to read
- 21 Currently reading

Published
**1990**
by National Aeronautics and Space Administration, National Technical Information Service, distributor in [Washington, DC], [Springfield, Va
.

Written in English

- Elastic waves.,
- Flow distribution.,
- Prediction analysis techniques.,
- Pressure oscillations.,
- Propeller blade.,
- Unsteady aerodynamics.

**Edition Notes**

Other titles | Unsteady blade surface pressures on a large ... |

Statement | M. Nallasamy and J.F. Groeneweg. |

Series | NASA technical memorandum -- 103218. |

Contributions | Groeneweg, John F., United States. National Aeronautics and Space Administration. |

The Physical Object | |
---|---|

Format | Microform |

Pagination | 1 v. |

ID Numbers | |

Open Library | OL15405944M |

Journal of Pressure Vessel Technology; Journal of Solar Energy Engineering; Journal of Thermal Science and Engineering Applications; Journal of Tribology; Journal of Turbomachinery; Journal of Verification, Validation and Uncertainty Quantification; Journal of Vibration and Acoustics; Conference Proceedings. All Conference Proceedings; Browse. It is then shown that the fluctuating thrust of one blade and propeller vibratory shaft forces calculated by the present method agree well with experiments. A sample calculation is shown for pressure contours on a blade surface with varying angular position in a nonuniform flow. Availability: Find a library where document is available.

local panel area and the normal, the pressure force can be calculated and integrated on the body. For a more detailed description of the numerical method, see [7]. Propeller model The propeller model used here is in detail described in [8], where a validation and an application example is given. Because of the advanced propeller modeling. Saeed Farokhi Curriculum Vita 6/20 "Blade Surface Pressure Measurement on a Pusher Propeller in Flight," (with Mordechai Vertzberger), SAE Transactions, Journal of Aerospace, Vol. 98, Section 1, , "System Design Aspects of Propulsion Education in Aerospace Engineering Curricula,".

Measurement of unsteady blade surface pressure on a single rotation large scale advanced prop-fan with angular and wake inflow at mach numbers from to [microform] [] Bushnell, P. [Washington, DC]: National Aeronautics and Space Administration, []. Validation and Pilot Applications of Unsteady CFD Simulations for (Blade) surface pressure APSIM acoustic far-field URANS Code (TAU) Perturbation First large-scale application of propeller simulation experience with TAU to fully realistic and very complex geometry.

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