Results 91 to 100 of about 101,352 (285)

Finite-rate water condensation in combustion-heated wind tunnels [PDF]

open access: yes
A quasi-one-dimensional method for computing finite rate nucleation and droplet growth of water in a supersonic expansion of combustion products is presented. Sample computations are included for the Langley 8 foot High Temperature Tunnel, but the method
Erickson, Wayne D.   +2 more
core   +1 more source

Research of the sonic-boom problem [PDF]

open access: yes
Wind tunnel tests were conducted to determine the characteristics of sonic booms. A theoretical examination of nonlinear effects in near and far flow fields, as well as sonic boom shock strength, is reported.
Drougge, G.
core   +1 more source

A Review of Flow Control Strategies for Supersonic/Hypersonic Fluid Dynamics

open access: yesAerospace Research Communications
Supersonic and hypersonic flows have gained considerable attention in the aerospace industry in recent years. Flow control is crucial for refining the quality of these high-speed flows and improving the performance and safety of fast aircraft. This paper
Shibo Lee   +9 more
doaj   +1 more source

Structure Design of the Force Testing Central Support of a Transonic and Supersonic Wind Tunnel

open access: yesJixie chuandong, 2015
The force testing central support is an important part of the model supporting system in a transonic & supersonic wind tunnel,the performance of which is qualified or not would directly affect the control of model attitude angel during wind tunnel ...
Dong Bin   +3 more
doaj  

Experimental Investigation of the Performance of a Novel Ejector–Diffuser System with Different Supersonic Nozzle Arrays

open access: yesFluids
The supersonic–supersonic ejector–diffuser system is employed to suck supersonic low-pressure and low-temperature flow into a high-pressure environment.
Dachuan Xu   +3 more
doaj   +1 more source

Suitableness of SLM Manufactured Turbine Blade for Aerodynamical Tests. [PDF]

open access: yesMaterials (Basel), 2023
Telega J   +4 more
europepmc   +1 more source

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