津贴
发表于 2025-3-25 03:40:01
https://doi.org/10.1007/978-981-15-9601-8Aerodynamics of Aerospace Vehicles; Conceptual Design of Aircraft; Turbomachinery Flows; Intake Aerodyn
Interregnum
发表于 2025-3-25 11:01:59
http://reply.papertrans.cn/27/2686/268548/268548_22.png
DRAFT
发表于 2025-3-25 13:45:26
S. Kishore Kumar,Indira Narayanaswamy,V. RameshCovers aerodynamics of aerospace vehicles.Special focus on Stealth in Aerospace Design.Looks at all aspects vehicle and propulsion system design
elucidate
发表于 2025-3-25 16:56:25
http://reply.papertrans.cn/27/2686/268548/268548_24.png
Innocence
发表于 2025-3-26 00:03:44
2195-4356 signThis book presents selected papers presented in the Symposium on Applied Aerodynamics and Design of Aerospace Vehicles (SAROD 2018), which was jointly organized by Aeronautical Development Agency (the nodal agency for the design and development of combat aircraft in India), Gas-Turbine Resear
Firefly
发表于 2025-3-26 04:04:28
https://doi.org/10.1007/978-3-8348-8116-8etric study is carried out for supersonic flow past a compression–decompression ramp (CDR), to determine the ramp inclination angle that minimizes the adverse effect of separated flow. The inclination angle below which weak interaction occurs is obtained from the numerical simulations.
我不重要
发表于 2025-3-26 07:32:16
,Parametric Study of Turbulent Flow Past a Compression–Decompression Ramp,etric study is carried out for supersonic flow past a compression–decompression ramp (CDR), to determine the ramp inclination angle that minimizes the adverse effect of separated flow. The inclination angle below which weak interaction occurs is obtained from the numerical simulations.
CORD
发表于 2025-3-26 09:26:38
Ermittlung von Zinsstrukturkurventitude variation on the aerodynamics of the launch vehicle during hot separation. Two different trajectories (or altitudes) are studied and the effect on the aerodynamic coefficients is quantified. The paper presents in detail about the simulated conditions, the variation in aerodynamic coefficients and the complex flow-field involved.
Ointment
发表于 2025-3-26 12:55:19
http://reply.papertrans.cn/27/2686/268548/268548_29.png
披肩
发表于 2025-3-26 16:53:38
Ermittlung von Zinsstrukturkurven vehicle configuration in the presence of launch pad and umbilical tower (UT). It is seen that the aerodynamic characteristics are significantly influenced by the presence of wind tunnel walls. Even though the model blockage is 4%, variation of 8.5% is seen in total force coefficients.