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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

HYPERSONIC VISCOUS FLOW OVER A SLENDER CONE. III. LAMINAR INSTABILITY AND TRANSITION.DEMETRIADES A.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 7TH FLUID PLASMA DYN. CONF.; PALO ALTO, CALIF.; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 535; PP. 1-9; BIBL. 10 REF.Conference Paper

INFLUENCE OF MODERATE WALL COOLING ON CONE TRANSITION AT ME=13.7 IN HELIUMFISCHER MC.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 4; PP. 282-283; BIBL. 14 REF.Serial Issue

BOUNDARY-LAYER INSTABILITY OBSERVATIONS AT MACH NUMBER 7.DEMETRIADES A.1977; J. APPL. MECH.; U.S.A.; DA. 1977; VOL. 44; NO 1; PP. 7-10; BIBL. 9 REF.Article

LAMINAR NATURAL CONVECTION OVER A SLENDER VERTICAL FRUSTRUM OF A CONE WITH CONSTANT WALL HEAT FLUXNA TY; CHIOU JP.1980; WAERME- U. STOFFUEBERTRAG.; DEU; DA. 1980; VOL. 13; NO 1-2; PP. 73-78; ABS. GER; BIBL. 11 REF.Article

COMPARISON OF THREE OSCILLATORY TECHNIQUES FOR CONES AT INCIDENCE = COMPARAISON DE TROIS TECHNIQUES OSCILLATOIRES POUR DES CONES EN INCIDENCEORLIK RUCKEMANN KJ; IYENGAR S; LABERGE JG et al.sdIN: AIAA 7TH AERODYN. TEST. CONF. PALO ALTO, CALIF., 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; NO 993; PP. 1-7; BIBL. 9 REF.Conference Paper

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