Results 31 to 40 of about 116 (92)
The influences of a variety of different physical phenomena are described as they affect the aerodynamic performance of turbine airfoils in compressible, high‐speed flows with either subsonic or transonic Mach number distributions. The presented experimental and numerically predicted results are from a series of investigations which have taken place ...
Phil Ligrani, Ting Wang
wiley +1 more source
Numerical Investigation of a Supersonic Wind Tunnel Diffuser Optimization
The objective of this study is to enhance the methodology for the design of a supersonic wind tunnel, improving the process with advanced computational techniques.
Riccardo Nicoletti +7 more
doaj +1 more source
DIGITAL DATA GATHERING SYSTEM, BLOWDOWN WIND TUNNEL [PDF]
Presented at ihe Ninth Meeting of the Supersonic Wind-Tunnel Assoc., Univ. of Southern Calif., and U. S. Naval Air Missile Test Center, Point Mugu, Calif., Apr. The Sandia 12 x 12-inch, transonic, blowdown tunnel facility is being equipped with a 10-channel digital datagathering system. The design and operation of ihe system are discussed. (W.J.H.)
openaire +2 more sources
Stress damage in operational natural gas venting pipes is a complex issue that requires pipeline designs tailored to specific operational conditions. This study aims to accurately predict operational stress during the blow‐off process by leveraging design and operational parameters to assess potential pipeline damage. Five machine learning (ML) methods—
Zhenning Fan +9 more
wiley +1 more source
We collected soil water percolation and nutrient flux at 60 cm depth to understand variability across topographic, soil texture and seasonal gradients within the remote Central Amazon region of Brazil. Main findings indicate percolation volume and solute concentration generally increase with decreasing elevation and clay content.
Jardel Ramos Rodrigues +13 more
wiley +1 more source
Prediction of total pressure characteristics in the settling chamber of a supersonic blowdown wind tunnel [PDF]
AbstractOccurrence of transient starting and stopping loads during tests at high Mach numbers is one of the major problems in intermittent blowdown wind tunnels. It is believed that in order to overcome this problem, the wind tunnel could be started at a low Mach number and low stagnation pressure; the desired high Mach number condition could be ...
G. K. Suryanarayana, S. R. Bhoi
openaire +1 more source
Spectral Energy of High-Speed Over-Expanded Nozzle Flows at Different Pressure Ratios
This paper addresses the long-standing question of understanding the origin and evolution of low-frequency unsteadiness interactions associated with shock waves impinging on a turbulent boundary layer in transonic flow (Mach: 1.1 to 1.3).
Manish Tripathi +5 more
doaj +1 more source
CONTROL OF REYNOLDS NUMBER IN A HIGH SPEED WIND TUNNEL. doi: 10.5028/jatm.2009.01016977
A conceptual control model for the Reynolds number test based on isentropic relations was established for the supersonic wind tunnel. Comparison of the system response of the model simulation and the actual wind tunnel test data was made to design the ...
Maurício G. Silva +2 more
doaj
Shock loss measurements in non-ideal supersonic flows of organic vapors. [PDF]
Conti CC +3 more
europepmc +1 more source
Application of a Gas-Kinetic BGK Scheme in Thermal Protection System Analysis for Hypersonic Vehicles. [PDF]
Zhou D, Du B, Guo T, Li Q, Lu Z.
europepmc +1 more source

