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  1. 321
    Izbor faktora rotacije vektora potiska za balističku raketu sa Lambertovim vođenjem / Choice of the rotational factor of the thrust vector for the ballistic missile with Lambert guidance
    by Danilo V. Ćuk
    Published 2008-04-01
    “... parameter for the thrust vector, the cut-off of the rocket engine can occur at zero angle of attack...”
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    Article
  2. 322
    Uticaj povećanja dometa na dinamičku stabilnost artiljerijskih raketa sa olučastim krilima / Influence of range extension on dynamic stability for artillery rockets with wrap around fins
    by Danilo Ćuk
    Published 2007-07-01
    “... of an artillery rocket with wrap around fins on its dynamic stability. The increased total impulse of the rocket...”
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    Article
  3. 323
    Wall Condensation Modelling in Convective Flow
    by Lejon, Marcus
    Published 2013
    “..., such as nuclear reactor containment, rocket engine nozzles and heat exchangers. The current study investigates...”
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  4. 324
    Radiation View Factors Between A Disk And The Interior Of A Class Of Axisymmetric Bodies Including Converging Diverging Rocket Nozzles
    by Murad, Mark Richard
    Published 2008
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  5. 325
    Rotating Detonation Combustor Mechanics
    by Anand, Vijay G.
    Published 2018
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  6. 326
    Large Eddy Simulations of the interactions between flames and thermal phenomena : application to wall heat transfer and combustion control
    by Maestro, Dario
    Published 2018
    “.... In a first part, wall heat transfer in a rocket engine sub-scale CH4/O2 burner isstudied...”
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  7. 327
    DETERMINATION OF THE THICKNESS OF THE COMPONENTS OF A DOUBLE-LAYER NICKEL-CHROMIUM COATING BY MAGNETIC PONDEROMOTIVE METHOD WITH UNILATERAL ACCESS TO THE CONTROLLED SURFACE
    by Y. V. Gnutenko, V. A. Rudnitsky
    Published 2017-12-01
    “... widely used to give the combustion chamber of a liquid-propellant rocket engine the required operational...”
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    Article
  8. 328
    H2-O2 supercritical combustion modeling using a CFD code
    by Benarous Abdallah, Liazid Abdelkrim
    Published 2009-01-01
    “... on liquid rocket engine performance. The necessity of raising rocket engines performance requires a...”
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    Article
  9. 329
    PARAMETRIC VIBRATION OF THE ROTOR TURBOPUMP ASSEMBLY ON BALL BEARINGS
    “... and as part of the turbopump assembly from a Liquid-Propellant Rocket Engine. The defects of ball bearings...”
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    Article
  10. 330
    MATHEMATICAL MODELING OF OMIC PROPULSION SYSTEM IN MICROSATELLITE GROUP FORMING
    “... rocket engine in the formation of a constellation of satellites. The limitations of the operating...”
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    Article
  11. 331
    Study on Thermal Degradation Characteristics and Regression Rate Measurement of Paraffin-Based Fuel
    “... rocket engine. The energy characteristics of paraffin-based fuel and HTPB fuel have been calculated...”
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    Article
  12. 332
    Numerical Study of the Working Process in the Reducing Gas Generator of the Upper Stage Oxygen - Methane Engine
    “...<p>This article deals with the problems of creating a reducing gas generator of the liquid rocket...”
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    Article
  13. 333
    Parametric study of manifolds using finite element analysis
    by Bäckström, Kristoffer
    Published 2008
    “... engines for the NGL. The environment of a rocket engine is extremely hostile, characterized by high...”
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  14. 334
    Dynamics Analysis and Testing of Gas-Pressurized Waterjet Rocket
    by Shiah, Wen-Goang, 夏文廣
    Published 1998
    “..., momentum equation, total kinetic power produced by the rocket engine...”
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  15. 335
    Investigation of passive control devices to suppress acoustic instability in combustion chambers.
    by Avandelino Santana Junior
    Published 2008
    “...Combustion instability problems have been experienced during nearly every rocket engine development...”
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  16. 336
    A systems study of very small launch vehicles
    “... rocket engine fabricated in silicon, and weighing 2 g. The engines use nitrogen tetroxide and hydrazine...”
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  17. 337
    Complex stress-strain behaviour of a cylindrical shell with a dynamically breaking internal elastic base
    “...During the operation of a solid-propellant rocket engine, the combustion products of a powder...”
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    Article
  18. 338
    Properties of a multi-layer multi-span corrugated package
    by R. I. Alkeev, V. I. Suslikov, I. D. Eskin
    Published 2020-07-01
    “..., hollow wide-chord blades of aircraft GTE fans, ring dampers of rocket engine rotors, as their damping...”
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    Article
  19. 339
    Studies on thermal stresses in elastic solids
    by Cheng, Che-Min
    Published 1952
    “..., in the combustion chamber of a rocket engine, where stresses produced by supporting seats are often too...”
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  20. 340
    Low-Thrust Perturbation Guidance
    by Bauer, Thomas Patrick
    Published 1982
    “... and elliptical. The only forces considered were the Sun's gravity and that of the constant thrust rocket engine...”
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