Flight investigation of a V/STOL transport model having six wing-mounted lift fans
Free flight tests in hoovering and forward flight free flight tests in hovering and forward flight lift fans
Grafton, S. B.↗
Engineering topics
Grafton, S. B.
Publications and source records attributed to Grafton, S. B..
Flight investigation of a V/STOL transport model with four pod-mounted lift fans
Flight characteristics of V/STOL transport model with four pod-mounted lift fans
Grafton, S. B.↗
Dynamic stability derivatives of a twin-jet fighter model for angles of attack from -10 deg to 110 deg
Dynamic stability derivatives of twin-jet fighter model for angles of attack from -10 deg to 110 deg
Grafton, S. B.↗
Investigation of lateral-directional dynamic stability of a tilt-wing V/STOL transport
Lateral-directional dynamic stability derivatives, characteristics, and handling qualities of tilt-wing V/STOL configuration
Chambers, J. R.↗
Static and dynamic stability derivatives of a model of a jet transport equipped with external-flow jet-augmented flaps
Static and dynamic stability derivatives of model jet transport equipped with external flow jet augmented flaps
Damato, R.↗
Static and dynamic longitudinal stability derivatives of a powered 0.18-scale model of a fan-in-wing VTOL aircraft
Static and dynamic longitudinal stability tests of fan in wing V/STOL aircraft model
Chambers, J. R.↗
Calculation of the dynamic longitudinal stability of a tilt-wing V/STOL aircraft and correlation with model flight tests
Aerodynamic factors, and effects on dynamic longitudinal stability characteristics of tilt wing V/STOL aircraft
Chambers, J. R.↗
Static and dynamic longitudinal stability derivatives of a powered 1/9-scale model of a tilt-wing V/STOL transport
Force tests to determine static and dynamic longitudinal stability derivatives of powered scale model of tilt-wing V/STOL transport aircraft
TILT-WING AIRCRAFT↗
A study to determine effects of applying thrust on recovery from incipient and developed spins for four airplane configurations
Effects of applying thrust along with optimum aerodynamic control surface defections on incipient and developed spin-recovery characteristics of four aircraft configurations
AERODYNAMIC STABILITY↗
Effects of aircraft relative density on spin and recovery characteristics of some current configurations
Relative density effect on spin and recovery characteristics of aircraft configurations
ATMOSPHERIC DENSITY↗