Publication Date:
2019-08-27
Description:
The present work discusses the results of some experimental studies on the possibility of attenuating shock waves in a supersonic flow. The shock waves were formed by an external source of electrical energy. An electromechanical method is described that permits partial recovery of the expended energy.
Keywords:
AERODYNAMICS
Type:
NASA-TM-77912
,
NAS 1.15:77912
Format:
application/pdf