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SOME FEATURES OF THE UNSTEADY PRESSURE FIELD IN TRANSONIC AIRFOIL BUFFETINGROOS FW.1980; J. AIRCR.; ISSN 0021-8669; USA; DA. 1980; VOL. 17; NO 11; PP. 781-788; BIBL. 17 REF.Article

HOT-FILM PROBE TECHNIQUE FOR MONITORING SHOCK-WAVE OSCILLATIONSROOS FW.1979; J. AIRCR.; USA; DA. 1979; VOL. 16; NO 12; PP. 871-875; BIBL. 6 REF.Article

DIRECT COMPARISON OF HOT-FILM PROBE AND OPTICAL TECHNIQUES FOR SENSING SHOCK-WAVE MOTIONROOS FW; BOGAR TJ.1981; AEROSPACE SCIENCES MEETING. 19 /1981-01-12/SAINT LOUIS MO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 6 P.; BIBL. 3 REF.Conference Paper

COMPARISON OF HOT-FILM PROBE AND OPTICAL TECHNIQUES FOR SENSING SHOCK MOTIONROOS FW; BOGAR TJ.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 8; PP. 1071-1076; BIBL. 4 REF.Article

SUPERCRITICAL AIRFOIL FLOWFIELD MEASUREMENTS.HURLEY FX; SPAID FW; ROOS FW et al.1975; J. AIRCR.; U.S.A.; DA. 1975; VOL. 12; NO 9; PP. 737-744; BIBL. 16 REF.Article

SUPERCRITICAL AIRFOIL FLOWFIELD MEASUREMENTS.HURLEY FX; SPAID FW; ROOS FW et al.1975; IN: ANN. INST. AERONAUT. ASTRONAUT. 8TH FLUID PLASMA DYN. CONF.; HARTFORD, CONN.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 880; PP. 1-9; BIBL. 16 REF.Conference Paper

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