Search
Issue: #2 (743)
Mechanical Engineering and Machine Science
Contour Machining Performance Improvement by Smoothing Spatial Piecewise Linear Toolpath and Quasi-Optimal Feed Rate Planning
Modeling the Process of Blades Shaping with Intraoperative Correction of Cutting Parameters
| Authors: Tanalin I.Sh. | |
Category: Mechanical Engineering and Machine Science | Chapter: Technology and Equipment for Mechanical and Physico-Technical Processing |
|
| Keywords: machining, gas turbine engine blade, adaptive control, mirror method, secant method | |
Optimization of Flat Grinding Modes for Low Rigidity Workpieces such as Rings and Prismatic Rods
Power, Metallurgic and Chemical Engineering
Forcing a Four-Stroke Engine by Switching it to a Two-Stroke Cycle at Low-Speed Modes
| Authors: Markov V.A., Barchenko F.B., Savastenko E.A., Savastenko A.A., Lotfullin Sh.R., Neverov V.A. | |
Category: Power, Metallurgic and Chemical Engineering | Chapter: Heat Engines |
|
| Keywords: gasoline engine, diesel engine, four-stroke cycle, two-stroke cycle, external speed characteristic, dynamic engine qualities | |
Combined Method for Calculating the Average Flow Centrifugal Compressor Stage
Aviation, Rocket and Technology
Aerodynamic Study of the Parachute Container Hatch Door with Various Design Parameters in its Separation from the Reentry Vehicle
Spacecraft Motion in an Ultra-Low Lunar Orbit under Lunar Gravitational Anomalies
| Authors: Arinchev S.V. | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture |
|
| Keywords: lunar gravitation anomalies, mass concentration, pseudo-random number, gravity-anomaly noise | |
Planet’s Real Motion Taken into Consideration in Analysis of an Interplanetary Trajectory Using Resonant with the Planet’s Orbit Segments
| Authors: Konstantinov M.S., Kurasbediani R.G. | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture |
|
| Keywords: interplanetary trajectory, sequence of gravity assist maneuvers, resonant orbit, pulse correction | |
Approximate Methodology for Design Ballistic Calculation of Two-Stage Launch Vehicles