au.\*:("PATE SR")
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COMPARISON OF NASA HELIUM TUNNEL TRANSITION DATA WITH NOISE-TRANSITION CORRELATION.PATE SR.1974; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 11; PP. 1615; BIBL. 4 REF.Article
RECENT ADVANCES IN THE PERFORMANCE AND TESTING CAPABILITIES OF THE AEDC-VKF TUNNEL F (HOTSHOT) HYPERSONIC FACILITY.PATE SR; EAVES RH JR.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 84; PP. 1-23; BIBL. 2 P.Conference Paper
DEVELOPMENT OF THE AEDC-VKF TUNNEL J. A REAL GAS HIGH DENSITY, TRUE VELOCITY, HYPERSONIC, AERODYNAMIC TEST FACILITYPATE SR; SILER LG; STALLINGS DW et al.sdIN: AIAA 7TH AERODYN. TEST. CONF. PALO ALTO, CALIF., 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; NO 993; PP. 1-22; BIBL. 11 REF.Conference Paper
THE ROLE OF COMPUTERS IN AERODYNAMIC TESTINGWHITFIELD JD; PATE SR; KIMZEY WF et al.1980; COMPUTERS AND FLUIDS; GBR; DA. 1980; VOL. 8; NO 1; PP. 71-99; BIBL. 53 REF.Article