Theoretical study of conditions limiting V/STOL testing in wind tunnels with solid floor
Conditions limiting V/STOL testing in wind tunnels with solid floors
Heyson, H. H.↗
Engineering topics
Heyson, H. H.
Publications and source records attributed to Heyson, H. H..
Theoretical study of the use of variable geometry in the design of minimal-correction V/STOL wind tunnels
Variable geometry design of minimal correction V/STOL wind tunnels
Heyson, H. H.↗
FORTRAN programs for calculating wind-tunnel boundary interference
FORTRAN programs for calculating wind tunnel boundary interference factors
Heyson, H. H.↗
Use of superposition in digital computers to obtain wind tunnel interference factors for arbitrary configurations, with particular reference to V/STOL models
Computer program for calculating wall interference factors of V/STOL aircraft and conventional airplanes
Heyson, H. H.↗
The flow throughout a wind tunnel containing a rotor with a sharply deflected wake.
Flow field throughout wind tunnel containing rotor with sharply defected blades, noting reversed flow effect in front of wake
Heyson, H. H.↗
Wind-tunnel wall effects at extreme force coefficients.
Wind tunnel wall constraints effects at extreme force coefficients during V/STOL testing shown different from effects in conventional aircraft testing
Heyson, H. H.↗
Some considerations in wind-tunnel tests of V/STOL models
Comparative evaluation of interference factor corrections in wind tunnel tests on vertical takeoff aircraft models
Heyson, H. H.↗
Wind Tunnel Wall Effects at Extreme Force Coefficients
Wind tunnel wall effects for highly deflected wakes
Heyson, H. H.↗
Experimental study of effects of electron irradiation from 20 keV to 1 MeV on a polyethylene terephthalate capacitor-type meteoroid detector
Electron irradiation from 20 keV to 1 MeV used to study effects on polyethylene terephthalate capacitor-type meteoroid detector
PARTICLE DETECTOR↗
Equations for the application of wind-tunnel wall corrections to pitching moments caused by the tail of an aircraft model
Mathematical expressions derived for application of wind tunnel wall corrections to pitching moments caused by tail of aircraft model
AIRCRAFT MODEL↗