Application of the method of characteristics to noncircular bodies at angle of attack
Method of characteristics for flow field analysis on elliptical winged body
Rakich, J. V.↗
Engineering topics
Rakich, J. V.
Publications and source records attributed to Rakich, J. V..
A method of characteristics for steady three- dimensional supersonic flow with application to inclined bodies of revolution
Characteristics method for determining three dimensional supersonic flow around inclined body of revolution
Rakich, J. V.↗
Theoretical and experimental study of supersonic steady flow around inclined bodies of revolution.
Three dimensional hypersonic steady flow around blunt and pointed cones at nonzero angles of attack calculated by method of characteristics
Cleary, J. W.↗
Three-dimensional flow calculation by the method of characteristics.
Characteristic method computer program for calculating three-dimensional supersonic flow around blunt and pointed bodies of revolution in reasonable time
SUPERSONIC FLOW↗
Investigation of methods for predicting flow in the shock layer over bodies at small angles of attack
Linearized characteristics method, and equivalent body method for predicting flow field about axisymmetric body at small angle of attack
AXISYMMETRIC BODY↗
A study of numerical methods for predicting flow about bodies at angle of attack
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Gallo, W. F.↗
The aerodynamic characteristics of several thick delta wings at Mach numbers to 6 and angles of attack 50 deg
Aerodynamic characteristics of thick delta wings at subsonic to supersonic speeds and angles of attack to 50 deg
DELTA WING↗
A theoretical and experimental study of hypersonic flow over flared bodies at incidence
Hypersonic flow over flared bodies at angle of attack
HYPERSONIC FLOW↗
A description of numerical methods and computer programs for two-dimensional and axisymmetric supersonic flow over blunt-nosed and flared bodies
Numerical methods and computer programs for two-dimensional and axisymmetric supersonic flow over blunt-nosed and flared bodies
AXISYMMETRIC FLOW↗
Calculation of hypersonic flow over bodies of revolution at small angles of attack.
First order yaw effects on hypersonic air flow about bodies of revolution
HYPERSONIC FLOW↗