Vortex-lattice FORTRAN program for estimating subsonic aerodynamic characteristics of complex planforms
Vortex-lattice FORTRAN program for estimating subsonic aerodynamic characteristics of complex planforms
Lamar, J. E.↗
Engineering topics
Margason, R. J.
Publications and source records attributed to Margason, R. J..
Review of propulsion-induced effects on aerodynamics of jet V/STOL aircraft
Propulsion device-induced effects on V/STOL aircraft aerodynamics in hover and transition flight
Margason, R. J.↗
Analysis of the flow field of a jet in a subsonic crosswind
Jet induced flow field effects on V/STOL aircraft in subsonic transition flight
Margason, R. J.↗
Jet-wake characteristics and their induced aerodynamic effects on V/STOL aircraft in transition flight
Jet-wake characteristics and aerodynamic effects on V/STOL aircraft
Fearn, R. L.↗
Analytic description of jet-wake cross sections for a jet normal to a subsonic free stream
Jet-wake cross section analysis for jet exhausting in free stream flow
Margason, R. J.↗
Aerodynamic Characteristics of Twin Propeller Deflected Slipstream STOL Airplane Model with Boundary Layer Control on Inverted V-tail
Aerodynamic characteristics of COIN aircraft model with boundary layer control on inverted V-tail
Gentry, G. L., Jr.↗
The path of a jet directed at large angles to a subsonic free stream
Path and shape of jet directed at large angles to subsonic free stream
Margason, R. J.↗
Aerodynamic characteristics of a five jet VTOL configuration in the transition speed range
Wind tunnel tests of a VTOL jet fighter to determine aerodynamic characteristics including stability
Gentry, G. L., Jr.↗
Computer program calculates wing aerodynamic characteristics for fixed wings with dihedral and variable-sweep wings at subsonic speeds
Vortex lattice is used to describe the lifting surface of an arbitrary wing planform in steady potential subsonic compressible flow in computer program which calculates wing aerodynamic characteristics. Estimates of flow field characteristics in the vicinity of a lifting wing can also be programmed.
Lamar, J. E.↗
Static calibration of an ejector unit for simulation of jet engines in small-scale wind-tunnel models
Static calibration of ejector unit for simulation of jet engines in small-scale wind tunnel models of VTOL aircraft
EJECTOR↗
Longitudinal stability and control characteristics of a powered model of a twin-propeller deflected-slipstream STOL AIRPLANE configuration
Longitudinal stability and control characteristics of powered model of twin-propeller deflected-slipstream STOL aircraft configuration
STOL AIRCRAFT↗
Jet-induced lift losses on VTOL CONFIGURATIONS hovering in and out of ground effect
Jet induced lift diminution on VTOL aircraft hovering in and out of ground effect
GROUND EFFECT↗
Jet-induced effects in transition flight
Performance characteristics of jet-powered VTOL FIGHTER aircraft in transition from hovering to forward flight
JET AIRCRAFT↗
Lateral control characteristics of a powered model of a twin-propeller deflected slipstream stol airplane configuration
Wind tunnel tests of static lateral and directional control of twin-propeller deflected slipstream STOL aircraft
DEFLECTION↗