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   journal of aerospace science and technology   
سال:2025 - دوره:18 - شماره:2


  tick  a simplify analytic approach for converting airplane and cantilever beams distributed loads to equivalent concentrated loads - صفحه:45-60

  tick  calibration of empirical coefficients in wake-oscillator model for vortex-induced vibrations using genetic algorithms - صفحه:35-44

  tick  effect of viscous heating on heat transfer and entropy generation inside a partially filled porous channel - صفحه:110-126

  tick  effects of syngas h2/co composition and turbulent intensity on the bluff-body premixed combustion characteristics - صفحه:1-16

  tick  evaluation of non-turbopump feed systems for application in a two-stage launch vehicle - صفحه:127-144

  tick  numerical study of flow pattern on a diamond wing-body equipped with lex at low angles of attack - صفحه:75-87

  tick  observability-guided autonomous path planning for quadrotor navigation in gnss-denied environments - صفحه:25-34

  tick  optimal orbital inclination based on maximum regional coverage criterion for a satellite in a low earth circular orbit - صفحه:145-157

  tick  quasi-static and dynamic analysis of a 12u cubesat under flight-phase environmental loads - صفحه:88-98

  tick  robust integrated guidance and control system for faulty actuator in two-dimensional pursuit engagements - صفحه:99-109

  tick  robust intelligent trajectory tracking for quadrotors: integrating backstepping and feedback-error-learning techniques - صفحه:61-74

  tick  spoofing attack detection in integrated gnss/ins navigation system using self-tuning kalman filter - صفحه:17-24
 

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