An investigation of transition fixing technique for a 10. 5% thick, 28 deg sweptback wing at high subsonic speeds and R approximately 3 million(Pressure distribution on sweptback wing at subsonic speeds noting boundary layer transition)
The effect of the electrogasdynamic factor on the development of small perturbations in a boundary layer on a thin profile(Vliianie elektrogazodinamicheskogo vozdeistviia na razvitie malykh vozmushchenii v pogranichnom sloe na tonkom profile)
Computation of the laminar near wake of a cylinder at a freestream Mach number of 6/by the Lees-Reeves method//Calcul du sillage proche laminaire d'un cylindre a Mach number of 6/par la methode de Lees-Reeves//(Laminar near wake of cylinder at free stream Mach 6, using modified Lees-Reeves method)
Some effects of Mach number on the transonic flutter characteristics of thin cantilever wings having a taper ratio 0. 6 and a sweptback angle of 45 deg(Mach number effect on flutter characteristics of thin cantilever wings analyzed in transonic blowdown wind tunnel, presenting results as flutter speed ratios)