Transient Solid-Propellant Burning Rate Model: Comparisons to Experimental Data | 東京工業大学附属図書館文献データベース

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Transient Solid-Propellant Burning Rate Model: Comparisons to Experimental Data

著者名:: D. Greatrix ( Ryerson University, Toronto, Canada )
掲載資料名:: AIAA meeting papers on disc
シリーズ名:: AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
シリーズ巻号:: 2006
発行年:: 2006
通号:: 2006-4426
ペーパー番号:: AIAA Paper 2006-4426
出版情報:: Reston, Va: American Institute of Aeronautics and Astronautics
ISSN:: 10877215
言語:: 英語
請求記号:: A07400/200618 [CD-ROM 2006 Disc 18]
資料種別:: テクニカルペーパー

詳細

TDL書誌ID:	ZA00047244
シリーズID:	PA00000151
会議名:	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
回次:	42nd
会議開催地:	Sacramento, California
会議開催年:	2006.07.09-2006.07.12

類似資料:

1 テクニカルペーパー Numerical Modeling Considerations for Transient Burning of Solid Propellants Greatrix, D. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー A STUDY OF COMBUSTION AND FLOW BEHAVIOUR IN SOLID-PROPELLANT ROCKET MOTORS Greatrix, D. R. National Aeronautics and Space Administration
2 テクニカルペーパー Numerical Transient Burning Rate Model for Solid Rocket Motor Simulations Greatrix, D. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Casting Process Effect on Composite Solid Propellant Burning Rate Ribereau,D., Breton,P.Le, Ballereau,S. American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Burning Rate Mechanisms of Solid Propellants. Experimental Study Lillo, F., D'Andrea, B., Marcelli, G., Tamburini, A. American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Nano Additives and Plateau Burning Rates in Composite Solid Propellants M. Stephens, E. Petersen, D. Reid, R. Carro, S. Seal American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Model for Prediction of Negative and Positive Erosive Burning D. Greatrix American Institute of Aeronautics and Astronautics	10 テクニカルペーパー A reverse engineering approack to modelling transient burning rate of solid rocket motors Kumar, V.R. Sanal, Raghunandan, B.N. American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Model for Predicting Fuel Regression Rate in Hybrid Rocket Engines D. Greatrix American Institute of Aeronautics and Astronautics	11 テクニカルペーパー An Ignition Transient Model for Solid Propellant Rocket Motors d'Agostino,L., Biagioni,L., Lamberti,G. American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Precision techniques for measuring burning rates of solid propellants during pressure transients Murphy, J.J., Martin, A.O., Krier, H. American Institute of Aeronautics and Astronautics	12 テクニカルペーパー SOLID PROPELLANT BURNING RATE MEASUREMENT METHODS USED WITHIN THE NATO PROPULSION COMMUNITY Fry,R.S., DeLuca,L., Gadiot,G., Frederick,R., Strecker,R., Besser,H-L, Whitehouse,A., Traineau,J-C, Ribereau,D., … American Institute of Aeronautics and Astronautics

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