Results 91 to 100 of about 101,352 (285)
Finite-rate water condensation in combustion-heated wind tunnels [PDF]
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
Study on dust control technology of mobile spray combined with full-section fog curtain in return airway of header working face. [PDF]
Jing D+5 more
europepmc +1 more source
Selection criteria of optimal conditions for supersonic tests in a blowdown wind tunnel [PDF]
Dijana Damljanović, Djordje Vuković
openalex +1 more source
Research of the sonic-boom problem [PDF]
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
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
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
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]
Telega J+4 more
europepmc +1 more source
Blockage Testing in the NASA Glenn 225 Square Centimeter Supersonic Wind Tunnel [PDF]
Abigail E. Sevier+2 more
openalex +1 more source