Turbine engine composite route flight loading spectrum derivation (Unknown)
- New search for: Song, Y.-d.
- New search for: Gao, D.-p.
- New search for: Song, Y.-d.
- New search for: Gao, D.-p.
In:
JOURNAL OF PROPULSION TECHNOLOGY -BEIJING-
;
21
, 112
;
54-56
;
2000
-
ISSN:
- Article (Journal) / Print
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Title:Turbine engine composite route flight loading spectrum derivation
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Contributors:Song, Y.-d. ( author ) / Gao, D.-p. ( author )
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Published in:JOURNAL OF PROPULSION TECHNOLOGY -BEIJING- ; 21, 112 ; 54-56
-
Publisher:
- New search for: JOURNAL OF PROPULSION TECHNOLOGY
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Publication date:2000-01-01
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Size:3 pages
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ISSN:
-
Type of media:Article (Journal)
-
Type of material:Print
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Language:Unknown
- New search for: 621.4
- Further information on Dewey Decimal Classification
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Classification:
DDC: 621.4 -
Source:
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Table of contents – Volume 21, Issue 112
The tables of contents are generated automatically and are based on the data records of the individual contributions available in the index of the TIB portal. The display of the Tables of Contents may therefore be incomplete.
- 1
-
Propulsion system stability control for super-maneuvering flightWang, L.-f. / Zhang, J. et al. | 2000
- 5
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Starting and accelerating the missile turbojet engine by ground testZheng, Y. et al. | 2000
- 9
-
Numerical investigation of the flow field inside the liquid hydrogen inducerYi, T.-x. / Cheng, F.-z. / Suo, Y.-s. et al. | 2000
- 12
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One-dimensional finite element solutions for liquid transients in propellant feedlinesCheng, M.-s. / Liu, K. / Zhang, Y.-l. et al. | 2000
- 16
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New sealing structure of high pressure liquid rocket engineDu, T.-e. et al. | 2000
- 20
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Effect of mixing tube area and position on performance for lobed ejectorWang, G.-z. / Wu, S.-s. / Wang, Z.-s. et al. | 2000
- 24
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Numerical simulation of plug nozzle flow fieldGuo, Z. / Liu, J. / Qu, Z.-h. et al. | 2000
- 27
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Numerical simulation of 3-D unsteady turbulent flow in SRM chamber with finocyl grainXiang, H.-j. / Fang, G.-y. et al. | 2000
- 32
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Numerical simulation of nonlinear gas oscillation in closed pipeLiu, J. / Guo, Z. / Qu, Z.-h. et al. | 2000
- 36
-
Numerical study on flow field in 2-D segment compression supersonic intake for an air-to-air missileWang, G.-h. / Li, J.-x. / Cai, T.-m. et al. | 2000
- 40
-
Numerical calculation for flow and heat transfer of a shrouder rotating disk with high-positioned air-inletXu, G.-q. / Zhan, G.-z. / Ding, S.-t. et al. | 2000
- 44
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Identification of nonlinear mathematic model of air pressure bufferYu, D.-r. / Shi, X.-x. / Yan, Z.-g. et al. | 2000
- 47
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Study for flow resistance characteristics of the modelled laminated porous wallYu, X.-h. / Dong, Z.-r. / Liu, S.-l. et al. | 2000
- 51
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Effect of temperature and rotational speed on radial clearance of turbine blade tipGuo, S.-f. / Xu, B. et al. | 2000
- 54
-
Turbine engine composite route flight loading spectrum derivationSong, Y.-d. / Gao, D.-p. et al. | 2000
- 57
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Calculating Hopf bifurcation point of a nonlinear rotor-bearing systemZhang, X.-j. / Xia, S.-b. / Wu, X.-h. et al. | 2000
- 60
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Calculation for effect of variable specific heat capacity on nozzle flow field and performanceWang, Z.-x. / Wang, J.-f. / Tang, D.-y. et al. | 2000
- 63
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Hypergolic propellant rocket engine combustion instability studies (text in English)Nie, W.-s. / Zhuang, F.-c. et al. | 2000
- 66
-
Incomplete combustion test for solid rocket motorsHan, Y. et al. | 2000
- 69
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Non-linear constitutive equation of HTPB composite solid propellantZhang, Y.-j. / Zhao, G.-h. / Yang, J.-h. et al. | 2000
- 73
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Chelated titanate aids used in nitrate plasticized polyether propellantLi, H.-x. / Deng, J.-r. / Tang, H.-x. et al. | 2000
- 77
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Effect of ethanolamine derivative aids on rheological properties of HTPB propellant slurryLu, G.-l. / Wang, B.-h. et al. | 2000
- 81
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Fibre-optic image viewing system applied to combustion testLi, M. / Song, W.-y. / Ji, Z.-y. et al. | 2000
- 85
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Simulated tests and data acquisition system for aerospike nozzleDai, W.-y. / Liu, Y. / Cheng, X.-c. et al. | 2000