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Effects of Crescent Shaped Block Width and Length on Flow Field and Film Cooling Performance.
- Published in:
- Trends in Sciences, 2023, v. 20, n. 7, p. 1, doi. 10.48048/tis.2023.5339
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- Article
CONCEPTUAL DESIGN AND STUDY OF FLOW THROUGH A DUAL BELL NOZZLE AT DIFFERENT ALTITUDES USING COMPUTATIONAL FLUID DYNAMICS.
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- i-manager's Journal on Mechanical Engineering, 2021, v. 11, n. 3, p. 39, doi. 10.26634/jme.11.3.18057
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- Article
Thermokinetic Analysis and Performance Evaluation of Guanidinium Azotetrazolate Based Gas Generating Composition for Testing of Solid Rocket Motor Nozzle Closures.
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- Propellants, Explosives, Pyrotechnics, 2018, v. 43, n. 10, p. 1006, doi. 10.1002/prep.201800103
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- Article
An improved constant volume cycle model for performance analysis and shape design of PDRE nozzle.
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- Applied Mathematics & Mechanics, 2018, v. 39, n. 2, p. 193, doi. 10.1007/s10483-018-2294-6
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- Article
Numerical Studies on Thrust Augmentation in High Area Ratio Rocket Nozzles by Secondary Injection.
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- Journal of Applied Fluid Mechanics, 2017, v. 10, n. 6, p. 1605, doi. 10.29252/jafm.73.245.27309
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- Article
Development of a Near-field Intensity Measurement Capability for Static Rocket Firings.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 9
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- Article
Integration strategy of on-machine measurement (OMM) and numerical control (NC) machining for the large thin-walled parts with surface correlative constraint.
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- International Journal of Advanced Manufacturing Technology, 2015, v. 80, n. 9-12, p. 1721, doi. 10.1007/s00170-015-7046-x
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- Article
COMPUTATIONAL AND EXPERIMENTAL STUDY ON SUPERSONIC FILM COOLING FOR LIQUID ROCKET NOZZLE APPLICATIONS.
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- Thermal Science, 2015, v. 19, n. 1, p. 49, doi. 10.2298/TSCI120908077P
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- Article
THERMOCHEMICAL ABLATION OF CARBON/CARBON COMPOSITES WITH NON-LINEAR THERMAL CONDUCTIVITY.
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- Thermal Science, 2014, v. 18, n. 5, p. 1625, doi. 10.2298/TSCI1405625L
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- Article
Numerical investigation of separation pattern and separation pattern transition in overexpanded single expansion ramp nozzle.
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- Aeronautical Journal, 2014, v. 118, n. 1202, p. 399, doi. 10.1017/S0001924000009192
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- Article
Experimental Identification of Thrust Components Imparted by an Electrodeless Helicon Plasma Thruster.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 1
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- Article
Performance Characterization of a Helicon Plasma Thruster with Annular Magnet.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 5
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- Article
2-DOF Angle Measurement of Rocket Nozzle with Multivision.
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- Advances in Mechanical Engineering (Sage Publications Inc.), 2013, v. 5, p. 1, doi. 10.1155/2013/942580
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- Article
Inverse Problem of Rocket Nozzle Throat for Estimating Inner Wall Heat Flux by Broydon-Fletcher-Goldfarb-Shanno & Conjugate Gradient Method.
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- International Review of Mechanical Engineering, 2011, v. 5, n. 5, p. 908
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- Article
Aerospike Rockets for Increased Space Launch Capability.
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- Air & Space Power Journal, 2011, v. 25, n. 2, p. 65
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- Article
Rocket nozzle payload design for a high-altitude student platform.
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- International Journal of Mechanical Engineering Education, 2008, v. 36, n. 3, p. 235, doi. 10.7227/IJMEE.36.3.7
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- Article
Theoretical modelling of digital radiographs of composite rocket nozzles for the analysis of defects.
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- Insight: Non-Destructive Testing & Condition Monitoring, 2007, v. 49, n. 10, p. 595, doi. 10.1784/insi.2007.49.10.595
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- Article
A STUDY ON THE THERMAL VIBRATION ANALYSIS OF THE GRAPHITE DISK UNDER THERMAL SHOCK.
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- International Journal of Modern Physics B: Condensed Matter Physics; Statistical Physics; Applied Physics, 2006, v. 20, n. 25-27, p. 4105, doi. 10.1142/S0217979206040933
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- Article
Near net-shape, ultra-high melting, recession-resistant ZrC/W-based rocket nozzle liners via the displacive compensation of porosity (DCP) method.
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- Journal of Materials Science, 2004, v. 39, n. 19, p. 6005, doi. 10.1023/B:JMSC.0000041697.67626.46
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- Article
Shock-Wave Egress from a Nozzle into a Bounded Space.
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- Doklady Physics, 2002, v. 47, n. 12, p. 856, doi. 10.1134/1.1536215
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- Article