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Approbation of the numerical model of account of viscosity impact on the flow in low-thrust rocket engine nozzles in the approximation of a laminar boundary layer with sliding
Shustov S.A.
Tests of tubing made of aluminum alloy 1953T1 with wear-resistant thread-lined coats
Ivanova A.V.
Improving the accuracy of assessing the position deviation in coordinate measurements of GTE compressor and turbine blade profiles
Bolotov M.A., Pechenin V.A., Ruzanov N.V.
Model for evaluating the end runouts of a rotor with parallel connections of parts
Grachev I.A., Kudashov E.V., Bolotov M.A., Pronichev N.D.
Providing carrier rocket motion controllability on the basis of design smoothed wind profile application
Yendutkina Y.A., Titov B.A.
Analysis of control programs and flight paths of a hypersonic vehicle in climb
Balakin V.L., Krikunov M.M.
Alignment and study of prototypes of the Offner hyperspectrometer
Karpeev S.V., Khonina S.N., Murdagulov A.R., Petrov M.V.
Development of the information technology for estimation of fundus image geometric parameters
Kuprijanov A.V., Ilyasova N.Y.
Comparative research of algorithms of measuring the geometry of complex profiles of gas turbine engine compressor blades
Pechenin V.A., Bolotov M.A., Ruzanov N.V., Stepanova E.R.
Assuring the durability of transport aircraft structure in multipurpose use based on the results of endurance and flight tests
Fomichev P.A., Kleptsov V.I.
Approaches to parametric models of blade machines formation
Shabliy L.S., Popov G.M., Kolmakova D.A.
Compressor blade profile reverse-engineering: building of middle curve and symmetrical profile
Shabliy L.S.
Gas-dynamic losses in the flow part of the channel charge of a solid-propellant rocket engine
A. N. Sabirzyanov A.N., Khamatnurova C.B., Kuzmin V.V.
To the question of cooling power components of radio-electronic equipment by impinging freon jets
Lopatin A.A., Gortyshov Y.F.
1 - 14 of 14 Items

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