LIBRARY OF CONGRESS WASHINGTON D C AEROSPACE TECHNOLOGY DIV
The mechanism of the process of liquid flow towards a rotor under reduced feed regimes is exaimined. A postulate is introduced for maintaining the angle of attack of the incoming flow under these regimes. The solution of this problem permits a rational approach to optimizing a number of the geometric parameters of impellers, presently determined on the basis of far-fromprecise, purely experimental recommendations. Author
ATD work assignment no. 88,
O Rabote Nasosov i Vozdukhoduvnykh Mashin na Rezhimakh Ponizhennykh Podach, trans. of Teploenergetika (USSR) v12 n10 p71-4 1965.