1-21 of 21 Books
Development of in-fiber reflective Bragg gratings as shear stress monitors in aerodynamic facilities
Development of in-fiber reflective Bragg gratings as shear stress monitors in aerodynamic facilities
By Devendra S. Parmar
Skin-friction measurements in a 3-D, supersonic shock-wave/boundary-layer interaction
Skin-friction measurements in a 3-D, supersonic shock-wave/boundary-layer interaction
By Aerospace Sciences Meeting & Exhibit (32nd 1994 Reno, Nev.)
Boundary-layer transition and global skin friction measurement with an oil-fringe imaging technique
Boundary-layer transition and global skin friction measurement with an oil-fringe imaging technique
By Daryl J. Monson
Application of Navier-Stokes code PAB3D with k-e turbulence model to attached and separated flows
Application of Navier-Stokes code PAB3D with k-e turbulence model to attached and separated flows
By Khaled S. Abdol-Hamid
Feasibility of generating an "artificial" burst in a turbulent boundary layer
Feasibility of generating an "artificial" burst in a turbulent boundary layer
By Mohamed Gad-el-Hak
Instrumentation development for study of Reynolds analogy in reacting flows
Instrumentation development for study of Reynolds analogy in reacting flows
By Dianne J. DeTurris
Shock tunnel studies of scramjet phenomena 1994
Shock tunnel studies of scramjet phenomena 1994
By R. G. Morgan
Shock tunnel studies of scramjet phenomena 1995
Shock tunnel studies of scramjet phenomena 1995
By R. G. Morgan
Analysis and evaluation of an integrated laminar flow control propulsion system
Analysis and evaluation of an integrated laminar flow control propulsion system
By Theodore G. Keith
A proof of concept experiment for reducing skin friction by using a micro-blowing technique
A proof of concept experiment for reducing skin friction by using a micro-blowing technique
By Danny P. Hwang
Further developments of the fringe-imaging skin friction technique
Further developments of the fringe-imaging skin friction technique
By Gregory G. Zilliac
Computational study of surface tension and wall adhesion effects on an oil film flow underneath an air boundary layer
Computational study of surface tension and wall adhesion effects on an oil film flow underneath an air boundary layer
By Alan Celić
Some experimental observations of the law of the wall behind large-eddy breakup devices using servo-controlled skin friction balances
Some experimental observations of the law of the wall behind large-eddy breakup devices using servo-controlled skin friction balances
By V. D. Nguyen
Dual cylindrical wave laser-Doppler method for measurement of skin friction in fluid flow
Dual cylindrical wave laser-Doppler method for measurement of skin friction in fluid flow
By Amir Ahmad Naqwi
Skin friction determination by LDV measurements in a viscous sublayer - analysis of systematic errors
Skin friction determination by LDV measurements in a viscous sublayer - analysis of systematic errors
By F. Leprince
A method for the approximate calculation of the skin friction coefficient of horizontal wavy plates
A method for the approximate calculation of the skin friction coefficient of horizontal wavy plates
By F. Nagel
Aircraft drag prediction and reduction: computational drag analyses and minimization; mission impossible?
Aircraft drag prediction and reduction: computational drag analyses and minimization; mission impossible?
By J. W. Slooff
An analysis code for the Rapid Engineering Estimation of Momentum and Energy Losses (REMEL)
An analysis code for the Rapid Engineering Estimation of Momentum and Energy Losses (REMEL)
By Lawrence J. De Chant
Evaluation of heated film sensors for the measurement of wall shear stress
Evaluation of heated film sensors for the measurement of wall shear stress
By Yves Drolet
Hydrodynamic aspects of shark scales
Hydrodynamic aspects of shark scales
By William G. Raschi
Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport
Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport
By Milton Lamb