Диссертация (531291), страница 34
Текст из файла (страница 34)
113–117.229. Cottney D.J., Ewins D.J. Towards the efficient vibration analysis ofShrouded Bladed disk assemblies // ASME Paper. – 1973. – №73 DEC – 144. –16p.255230. Courent R. Varitional methods for the solution of problem of equilibrium and vibration // Bul.Amer. Math. Soc. – 1943. – V. 96. – P. 1054–1059.231. Elchuri V., Gallo A.M., Skalski S.C. Forced vibration analysis of rotating cyclic structures in NASTRAN // NASA Contractor Report. – 1983.
– CR165429. – 174p.232. Elchuri V., Smith G.C.C., Gallo A.M. NASTRAN Forced vibrationstresis of rotating cyclic structures // J. of vibration stress and reability in design.– 1983. – №83. – P. 1–11.233. Ewins D.J. Bladed discs vibtration .// A review of techiques and characteristics.
Proc. Int. Conf. On Recent Advances in Structural Dynamics. Southamption. – 1980. V.1. – P. 187–210.234. Ewins D.J., Imregun M. Vibtration modes of packeted bladed discs //Vibtration of Bladed Discs Assemblies (9-th Bienial Conf. On Mechanical Vibration and Noist-Dearborn. 11–14 Sep., 1983). – Michigan, 1983. – P. 231–234.235. Grammel R.
Drillungs und dehnungs schwingen von scheiben //Zeitschrift für angew. – Math. und Mech. – 1925. – №5. – S. 192–200236. Henry R. Contribution a l’etude dynamique des machines tournautes:Dis. … Dr. Ing. – Unuversite Claude Bernard. – Lyon, 1981. – 156p.237. Henry R., Lalanne M.
Vibration a1nalysis of rotating compressorblades. Jornalof Engenering for Indastry, August 1974.238. Hofmeister L.D., Evenson D.A. Vibration problems using isoparametric shell elements // Int. J. for Num. Mech. in Eng., 1972. – V. 5. – P. 142–145.239. Hohlrieder M. Zur statischen und dynamischen Analyse rotierenderelastischen (Turbinenschaufelen, Verdichter) bei transienten Betriebsbedingungen: Dis. … Dr. Ing.
– Kassel, 1994. – 202s.240. Humilton E.B., Alan L. Methods and apparatus for analysing variationsin rotary moution: G01b7/14/ №9609677.1256241. Irretier H. Berechnung der Schwingungen rotierender beschaufelterScheiben mitels eines anfangswertverfahrens: Dis. … Dr. Ing.
– Hannover,1978. – 129s.242. Irretier H., Hohlrieder M. Transiente Schevingungen von Turbinenschaufelen, DFG-Abschlußbericht, Institut für Mechanik, Universität Gh Kassel,1991. – 184s.243. Janecki S., Krawczuk M. Dynamics of Steam Turbine Rotor Blading. –Gdansk, 1998. – 382p.244. Kirchberger G., Paulum J.-H.
Berechnug von Eigenfrequenzen derShaufel-pakete in Dampf-und Gasturbinen insbesoundere bei verjüngten Schaufeln // Konstruktion. – 1958. – Bd.10, №2. – S. 41–50.245. Kirkhope J., Wilson G.P. A finite element analysis for the vibrationmodes of a bladed disc // J. of sound and vibration. – 1976. – V.49, №4. – P.469–482.246. Kirkhope J., Wilson G.P. Analysis of coupled bladed disk vibration inaxial flow turbine and fan // Structures , Struct. Dyn. Mater.: Proc. 12thAIAA/ASME Conf. – ASME paper N 71–375. – 1971.
– P. 1–11.247. Leissa A.W. Vibrations aspect of rotation turbomashinary blades // Applied Mechanics Reviews. – 1981. – V.34, №5. – P. 629-635.248. Leissa A.W. Vibration of turbine engine Blades by Shells analysis // J.Shock and Vibration Digest. – 1980. – V.12, №5. – P. 153–162.249. Mac Neal R.H. A simple quadrilateral shell element // Cumputers andstructures. – 1978. – V.8, №2. – P. 175–183.250.
Macbain J.C., Genin J. Effect of support flexibility on the fundamentalfrequency of vibrating beams // J. of Franclin Institute. – 1973. – V. 296, №4. –P. 259–273.251. Maillardet P., Hoffman D.A.,Norman M.E. A new tool for designingquit, low vibration main propulsion gears. Paper 20, INEC 96, Warship design:what to do? Newcastle, UK, 1996.257252. Mark W.D. Use of the generalized transmission error in the equationsof motion of gear system. ASME Trans.1. Mech. Trans Auto.in Des.
1987. –109, p.283.253. Mazurkiwicz M. Oblicszenia premieszczen, czesmosci i postaci dragnwlasnych lopatec maszyn wirnikowych metoda elementow skonszonych //Archiwum bydowy maszyn. – 1980. – V.27, N4. – P. 427–447.254. Modal testing of rotating machinery while it is operating / MarscherWilliam D. // J. Sound and Vibration. – 1999.- 33 № 11. – P. 29 – 32.255.
Modeling interfacial condition in normally flat contacts for applicationto fretting fatigue of turbine engine components / McVeigh P.A., Harish G., Farris T.N., Szolwiski M.P. // int. J. Fatigue. – 1999. – 21, Suppl. – P. 157–165.256. Olson M.D., Lindberg G.M. Dynamic analysis of shallow shell with adouble-cuvired triangular finite element // J. Sound and Vibration. – 1971.
– V.19, №3. – P. 299–318.257. Olson M.D., Lindberg G.M. Vibration analysis of cantilevered curvedplates using a new cylindrical shell finite element // 2nd Conf. on Mart. Meth. inStruct. Mech. Wright- Patterson A.F. Base. – Ohio, 1968. – P. 247–270.258. Parisch H. A critical survey the 9–node degenerated schell elementwith special emphasis on thin schell application and reduced integration //Comp. Meth. Appl. Mech. and Eng. – 1979. – V.
20. P. 323–350.259. Ramamurti V., Kielb K. Natural frequencies of twisted rotating plates //J. Sound and Vibration. – 1984. – V.94, №3. – P. 429–449.260. Rao J.S. Turbomaschine blade vibration // 5th world Congr. Theor.Mach. and Mech. – 1979. V.1. – P. 637–640.261. Resonance charaacteristics of turbine blades with compaund periodicstructure / Saito Eiji, Namura Kiyoshi, Okabe Akira // JSME Int. J.B. –1998.
–41, №3. – P. 727–733.262. Riehm S. Schwingungen freistehender ND–Endschaufeln einer Kondensationsturbine im Ventilationsberieb: Dis. … Dr. Ing. – Stuttgart, UNI, 1997.– 119s.258263. Riger N.F. Finite element analysis of turbomachine blade problems //Finite Element Applications in vibration Problems: The Design. EngineeringTechnical Conf. Chicago, Illinois. 26–28 Sep. – 1977. – P. 143–254.264. Rzadkowski R. Free Vibration of Tuned and Mistuned Bladed Disc:Report № 306/1252/90, Polish Academy of Science.
– Gdansk, Poland, 1990. –P. 42–49.265. Sagendorph F.E. Natural frequencies of mid–span shrouded fan blades// Struct. din. asp. of bladed disc assemblies: publ. ASME. – New–York. – 1976.– P. 93–99.266. Salame A.M. Finite element dynamic analysis of blade packets andbladed disc assemblies: Ph. D.
Thesis. University of Southamption. – 1977. –184p.267. Salame A.M., Petyt M. Dynamic responce of packets of blades by thefinite element method // ASME Paper 77-DET-70. – 1977. – 17p.268. Schaufelschwingunge erfassen // BWK: Brenst. – Warme–Kraft. –2000. – 52, №1–2. S.56.269. Seager D.L. Condition for neutralization of excitation by the teeth inepicyclical gearing. Journal Mechanical Engineering Science, Mech, E. 1975. –Vol 17 №5 p.293 – 298.270. SOLVIA SYSTEM 87: User Manual, Solvia Engineering AB, Scweden.
– 1987. – 146p.271. Srinivasan A.V., McFarland D.M. Characterization of laws of frictionin the context of engine blade dynamics // Trans. ASME. J. Eng. Gas Turbinesand Power. – 1998. – 120, №4. – P. 759–765.272. Stodola A. Über die schwingungen am dampfturbinen laufrädern.Schwiezervishe Bauzeitg. – 1914.
– №63. – S. 251–255 und 271–275.273. Stoekicht W.G. Journal of the American Sosiety of Naval Engineering1948, vol. 60.274. Surena K.S. Transition finite element for axisymmetric stress analysis //Int. J. for Num. Math. in Eng. – 1980. – V.15. – P. 809–832.259275. Surena K.S. Transition finite element for three dimensional stress analysis // Int.
J. for Num. Math. in Eng. – 1980. – V. 15. – P. 991–1020.276. Thompson S. J., Haigh J., Hofmann D.A., Rosinski J., Pennell J.A. Afour megawatt test rig for gear nois and vibration research // Proc. Int. Conf. onGearing and Power Transmissions, Newcastle, UK, 1994. – p.445 – 451.277. Tong J., Wang K.W. Vibration control of rotationally periodic stucturesusing passive piezoelectric shunt networks and active compensation // Trans.ASME. J.
Vibr. And Acoust. – 1999. – 121, №3. – P. 379–390.278. Trompette Ph., Lalanne M. Vibration analysis of rotating turbineblades. –A.S.M.E. Paper 74, WADE 23.279. Turcotte J.F., Hollkamp J.J., Gordon R.W. Vibration of a mistunedbladed–disk assembly using structurally damped beams // J. AIAA, 1998. –Vol.36, №12. – P. 2225–2228.280. Umemura S., Mase M., Kadoja Y. Vibration analysis of grouped bladesof turbines by the finite element method // Mitsubisi heavy Industries technicalreview.–1979.–V.16.–P.85–91.281. Vibration stress localization in turbomachine blades due to their complex geometry and effect of damage / Vorobiev Yu.S., Kanilo S.P., NikoulinaE.I. ets. // Proc 1997 ASME ASIA Conf.
And Exib. Techn. Paper ASME 97AA-020, Singapore ASME, New York, USA. – P. 369–374.282. Vorobjov Yu.S. Complex of methods and programs for static and vibrational calculations of turbomachine blading // U.S. – Ukrainian Energy Tradeand Investment Conf. – Kharkov, 1999. – P. 315.283. Vorobjov Yu.S., Kanilo S.P., Nikoulina E.I. Numerical investigation ofblade packet vibrations // Proc 1997 ASME ASIA Conf. And Exib.
![](https://s.studizba.com/z.php?f=/templates/si/i/noavatar.png&w=100&h=100&t=1"){kind=avatar}
