----------------- FILE NUMBER 1062----------------- 1. TITLE: CASE 8611; BACHALO, W. D., AND JOHNSON, D. A.; TRANSONIC TURBULENT BOUNDARY LAYER SEPARATION ON AN AXISYMMETRIC "BUMP" 2. REVISION DATE: FEBRUARY 12, 1981 3. EVALUATORS: HORSTMAN, C. C., AND RUBESIN, M. W.; NASA AMES RESEARCH CENTER MOFFETT FIELD, CA 94035 4. DATE AND LOCATION OF EXPERIMENT: 1978, NASA AMES, 2- BY 2-FOOT TRANSONIC WIND TUNNEL, NASA AMES RESEARCH CENTER, MOFFETT FIELD, CA 94035 5. ABSTRACT: THE EXPERIMENT WAS CONDUCTED IN THE AMES 2- BY 2-FOOT TRANSONIC WIND TUNNEL. THE FACILITY IS A CLOSED-RETURN, VARIABLE-DENSITY, CONTINUOUS RUNNING TUNNEL WITH 21% OPEN POROUS-SLOTTED UPPER AND LOWER WALLS. THE AXISYMMETRIC FLOW MODEL OF THIS INVESTIGATION CONSISTED OF AN ANNULAR CIRCULAR ARC BUMP AFFIXED TO A CIRCULAR CYLINDER ALIGNED WITH THE FLOW DIRECTION. THE AXIAL SYMMETRIC CONFIGURATION WAS CHOSEN TO CIRCUMVENT THE PROBLEM OF SIDEWALL BOUNDARY-LAYER CONTAMINATION OF TWO-DIMENSIONALITY THAT CAN OCCUR IN FULL-SPAN TWO-DIMENSIONAL TESTING. THE THIN-WALLED CYLINDER WAS 15.1 CM IN OUTSIDE DIAMETER AND EXTENDED 61 CM UPSTREAM OF THE BUMP LEADING EDGE. THE STRAIGHT SECTION OF THE CYLINDER PERMITTED NATURAL TRANSITION AND A TURBULENT BOUNDARY LAYER INCIDENCE ON THE BUMP OF SUFFICIENT THICKNESS TO ALLOW ACCURATE DETERMINATION OF THE BOUNDARY LAYER INFORMATION. HOWEVER, THE BOUNDARY LAYER WAS NOT SO THICK IN COMPARISON TO THE INTERACTION ON AIRFOILS SUCH THAT SEPARATION OF GREATER SEVERITY WOULD OCCUR THAN IS REPRE- SENTATIVE OF FULL SCALE. THE CIRCULAR-ARC BUMP HAD A 20.3 CM CHORD AND A THICKNESS OF 1.9 CM. ITS LEADING EDGE WAS JOINED TO THE CYLINDER BY A SMOOTH CIRCULAR ARC THAT WAS TANGENT TO THE CYLINDER AND THE BUMP AT ITS TWO END POINTS. TEST CONDITIONS WERE A FREE-STREAM MACH NUMBER OF 0.875 AND UNIT REYNOLDS NUMBER OF 13.1*(10)**6/M. AT THIS FREE-STREAM MACH NUMBER, A SHOCK WAVE WAS GENERATED OF SUFFICIENT STRENGTH (MP=1.32) TO PRODUCE A RELATIVELY LARGE REGION OF SEPARATED FLOW. THE SEPARATION AND REATTACHMENT POINTS WERE AT APPROXIMATELY 0.7 AND 1.1 CHORDS, RESPECTIVELY. BOUNDARY LAYER MEASUREMENTS WERE OBTAINED BY THE LASER VELOCIMETER TECHNIQUE FROM UPSTREAM OF SEPARATION THROUGH REATTACHMENT. THESE DATA CONSIST OF THE MEAN VELOCITIES AND TURBULENCE INTENSITIES IN THE STREAMWISE AND NORMAL DIRECTION. AND THE VELOCITY CORRELATION U1V1 SEPARATION AND REATTACH- MENT LOCATIONS WERE DETERMINED FROM OIL-FLOW VISUALIZATIONS AND LOCAL SURFACE STATIC PRESSURES WERE OBTAINED WITH CONVENTIONAL PRESSURE INSTRUMENTATION. 6. REFERENCES: BACHALO, W. D., MODARRESS, D., AND JOHNSON, D. A., "EXPERIMENTS IN TRANSONIC AND SUPERSONIC TURBULENT BOUNDARY LAYER SEPARATION," AIAA PAPER 77-47, LOS ANGELES, CA. 1977. BACHALO, W. D. AND JOHNSON, D. A., "AN INVESTIGATION OF TRANSONIC TURBULENT BOUNDARY LAYER SEPARATION GENERATED ON AN AXISYMMETRIC FLOW MODE," AIAA PAPER 79-1479, WILLIAMSBURG, VA, 1979. JOHNSON, D. A. AND BACHALO, W. D., "TRANSNOIC FLOW ABOUT A TWO-DIMENSIONAL AIRFOIL - INVISCID AND TURBULENT FLOW PROPERTIES," AIAA JOURNAL, VOL. 18, JAN. 1980, PP. 16-24. MCLAUGHLIN, D. K. AND TEIDERMAN, W. G., "BIASING CORRECTIONS FOR INDIVIDUAL REALIZATION OF LASER ANEMOMETER MEASUREMENTS IN TURBULENT FLOWS," PHYSICS OF FLUIDS, VOL. 16, DEC. 1973, PP. 2082-2088. JOHNSON, D. A., HORSTMAN, C. C., AND BACHALO, W. D., "A COM- PREHENSIVE COMPARISON BETWEEN EXPERIMENT AND PREDICTION FOR A TRANSONIC TURBULENT SEPARATED FLOW," AIAA PAPER 80-1407, SNOWMASS, COLO., 1980. 7. INSTRUMENTATION: LASER VELOCIMETER: THE LOCAL INSTANTANEOUS VELOCITY DATA WERE OBTAINED WITH A TWO-COMPONENT LASER VELOCIMETER SYSTEM FROM WHICH THE TURBULENT REYNOLDS STRESSES AND KINETIC ENERGIES WERE REALIZED, AS WELL AS THE LOCAL MEAN VELOCITIES. THIS SYSTEM UTILIZES TWO WAVE LENGTHS FROM AN ARGON-ION LASER TO MEASURE TWO ORTHOGONAL VELOCITY COMPONENTS SIMULTANEOUSLY. BRAGG-CELL FREQUENCY SHIFTING IS USED IN BOTH WAVE LENGTHS TO INSURE A SUFFICIENT NUMBER OF FRINGE CROSSINGS IN REGIONS OF HIGH TURBULENCE AND TO PROVIDE UNAMBIGUOUS SIGNAL INTERPRETA- TION IN REVERSE-FLOW REGIONS. WITH FORWARD-SCATTERED LIGHT COLLECTION, THE SYSTEM IS SUFFICIENTLY SENSITIVE THAT IT CAN OPERATE WITH ONLY THE NATURALLY OCCURRING PARTICLES IN THIS FACILITY. THESE PARTICLES, WHICH ARE THOUGHT TO BE CONDENSED OIL VAPOR DROPLETS ORIGINATING FROM THE DRIVE SYSTEM, ARE ESTIMATED TO BE 1 UM IN DIAMETER OR LESS, AS DETERMINED FROM MEASUREMENTS ACROSS A NORMAL SHOCK WAVE. THE EFFECTIVE SENSING VOLUME OF THE VELOCIMETER WAS ESTIMATED TO BE 200 UM IN DIAMETER AND 2 MM LONG; THE AXIS OF THE VOLUME WAS NORMAL TO THE FLOW DIRECTION. 8. EXPERIMENTAL PARAMETERS: MODEL: THE CIRCULAR ARC BUMP HAD A 20.3 CM. CHORD THICKNESS OF 1.9CM. ITS LEADING EDGE WAS JOINED TO THE CYLINDER BY A SMOOTH CIRCULAR ARC THAT WAS TANGENT TO THE CYLINDER AND THE BUMP AT ITS TWO END POINTS. TEST SECTION: THE EXPERIMENT WAS CONDUCTED IN THE AMES 2- BY 2-FOOT TRANSONIC WIND TUNNEL. THE THIN WALLED CYLINDER WAS 15.1CM IN OUTSIDE DIAMETER, AND EXTENDED 61CM UPSTREAM OF THE BUMP LEADING EDGE. RE- UNIT REYNOLDS NUMBER = 13.1(10**6) MACH- FREE-STREAM MACH NUMBER = 0.875 9. MEASURED AND INFERRED VARIABLES: X/C: NON-DIMENSIONAL STREAMWISE COORDINATE MEASURED FROM THE BUMP LEADING EDGE PTOT: TOTAL PRESSURE, N/M**2 Y: TRANSVERSE COORDINATE, M U: MEAN STREAMWISE VELOCITY, M/S U1: FREE-STREAM VELOCITY, M/S V: MEAN TRANSVERSE VELOCITY, M/S V1: TRANSVERSE FREE-STREAM VELOCITY, M/S U1V1: REYNOLDS STRESS, M**2/S**2 TKE: KINETIC ENERGY THICKNESS PW: WALL STATIC PRESSURE 10. MEASUREMENT UNCERTAINTY: NONE PROVIDED 11. TAPE ORGANIZATION: THE TAPE IS A 2400 FT., 9 TRACK, ODD PARITY, PHASE ENCODED, UNLABELLED TAPE WRITTEN AT A DENSITY OF 1600 BITS PER INCH ACCORDING TO EBCDIC CODE. THE RECORD FORMAT IS FIXED AND BLOCKED; RECORD LENGTH=80 BYTES, 100 RECORDS PER BLOCK; BLOCKSIZE=8000 BYTES. NORMALIZED DATA ARE CREATED FROM MEASURED DATA AS FOLLOWS: XNORM=(X-XMIN)/(XMAX-XMIN). THUS EACH NORMALIZED DATUM IS WRTTEN ONTO TAPE AS A VALUE BETWEEN 0.0 AND 1.0. ALL NULL DATA ARE WRITTEN AS 2.0. THE EQUATION DESCRIBING THE RELATION BETWEEN ACTUAL DATA AND THE NORMALIZED DATA ON THE TAPE IS X=XMIN + ((XMAX-XMIN)*XNORM) FILE # NREC CONTENTS FORMAT COMMENTS 1 CONTAINS ITEMS 1 TO 11 OF THIS WRITE-UP 2 33 X/C,PW/PTOT 2E16.3 RECORD 1: MAXIMUM VALUE X/C,PW/PTOT 2E13.6 RECORD 2: MINIMUM VALUE 3 15 Y,U/UTHETA,U1/UTHETA, 4E13.6 RECORDS 1-2 MAXIMUM V/UTHETA,V1/UTHETA, 3E13.6 VALUES -U1V1*1000/UTHETA**2, TKE*1000/UTHETA**2 Y,U/UTHETA,U1/UTHETA, 4E13.6 RECORDS 3-4 MINIMUM V/UTHETA,V1/UTHETA, 3E13.6 VALUES -U1V1*1000/UTHETA**2, TKE*1000/UTHETA**2. Y,U/UTHETA,U1/UTHETA, 7I6 RECORDS 5-15 V/UTHETA,V1/UTHETA, NORMALIZED VALUES -U1V1*1000/UTHETA**2, X/C = -0.250 TKE*1000/UTHETA**2 4 16 Y,U/UTHETA,U1/UTHETA, 4E13.6 RECORDS 1-2 MAXIMUM V/UTHETA,V1/UTHETA, 3E13.6 VALUES -U1V1*1000/UTHETA**2, TKE*1000/UTHETA**2. Y,U/UTHETA,U1/UTHETA, 4E13.6 RECORDS 3-4 MINIMUM V/UTHETA,V1/UTHETA, 3E13.6 VALUES -U1V1*1000/UTHETA**2, TKE*1000/UTHETA**2. Y,U/UTHETA,U1/UTHETA, 7I6 RECORDS 5-16 V/UTHETA,V1/UTHETA, NORMALIZED VALUES -U1V1*1000/UTHETA**2, X/C = 0.563 TKE*1000/UTHETA**2 5 14 Y,U/UTHETA,U1/UTHETA, 4E13.6 RECORDS 1-2 MAXIMUM V/UTHETA,V1/UTHETA, 3E13.6 VALUES -U1V1*1000/UTHETA**2, TKE*1000/UTHETA**2. Y,U/UTHETA,U1/UTHETA, 4E13.6 RECORDS 3-4 MINIMUM V/UTHETA,V1/UTHETA, 3E13.6 VALUES -U1V1*1000/UTHETA**2, TKE*1000/UTHETA**2. Y,U/UTHETA,U1/UTHETA, 7I6 RECORDS 5-14 V/UTHETA,V1/UTHETA, NORMALIZED VALUES -U1V1*1000/UTHETA**2, X/C = 0.625 TKE*1000/UTHETA**2 6 14 Y,U/UTHETA,U1/UTHETA, 4E13.6 RECORDS 1-2 MAXIMUM V/UTHETA,V1/UTHETA, 3E13.6 VALUES -U1V1*1000/UTHETA**2, TKE*1000/UTHETA**2. Y,U/UTHETA,U1/UTHETA, 4E13.6 RECORDS 3-4 MINIMUM V/UTHETA,V1/UTHETA, 3E13.6 VALUES -U1V1*1000/UTHETA**2, TKE*1000/UTHETA**2. Y,U/UTHETA,U1/UTHETA, 7I6 RECORDS 5-14 V/UTHETA,V1/UTHETA, NORMALIZED VALUES -U1V1*1000/UTHETA**2, X/C = 0.688 TKE*1000/UTHETA**2 7 19 Y,U/UTHETA,U1/UTHETA, 4E13.6 RECORDS 1-2 MAXIMUM V/UTHETA,V1/UTHETA, 3E13.6 VALUES -U1V1*1000/UTHETA**2, TKE*1000/UTHETA**2. Y,U/UTHETA,U1/UTHETA, 4E13.6 RECORDS 3-4 MINIMUM V/UTHETA,V1/UTHETA, 3E13.6 VALUES -U1V1*1000/UTHETA**2, TKE*1000/UTHETA**2. Y,U/UTHETA,U1/UTHETA, 7I6 RECORDS 5-19 V/UTHETA,V1/UTHETA, NORMALIZED VALUES -U1V1*1000/UTHETA**2, X/C = 0.750 TKE*1000/UTHETA**2 8 18 Y,U/UTHETA,U1/UTHETA, 4E13.6 RECORDS 1-2 MAXIMUM V/UTHETA,V1/UTHETA, 3E13.6 VALUES -U1V1*1000/UTHETA**2, TKE*1000/UTHETA**2. Y,U/UTHETA,U1/UTHETA, 4E13.6 RECORDS 3-4 MINIMUM V/UTHETA,V1/UTHETA, 3E13.6 VALUES -U1V1*1000/UTHETA**2, TKE*1000/UTHETA**2. Y,U/UTHETA,U1/UTHETA, 7I6 RECORDS 5-18 V/UTHETA,V1/UTHETA, NORMALIZED VALUES -U1V1*1000/UTHETA**2, X/C = 0.813 TKE*1000/UTHETA**2 9 18 Y,U/UTHETA,U1/UTHETA, 4E13.6 RECORDS 1-2 MAXIMUM V/UTHETA,V1/UTHETA, 3E13.6 VALUES -U1V1*1000/UTHETA**2, TKE*1000/UTHETA**2. Y,U/UTHETA,U1/UTHETA, 4E13.6 RECORDS 3-4 MINIMUM V/UTHETA,V1/UTHETA, 3E13.6 VALUES -U1V1*1000/UTHETA**2, TKE*1000/UTHETA**2. Y,U/UTHETA,U1/UTHETA, 7I6 RECORDS 5-18 V/UTHETA,V1/UTHETA, NORMALIZED VALUES -U1V1*1000/UTHETA**2, X/C = 0.875 TKE*1000/UTHETA**2 10 18 Y,U/UTHETA,U1/UTHETA, 4E13.6 RECORDS 1-2 MAXIMUM V/UTHETA,V1/UTHETA, 3E13.6 VALUES -U1V1*1000/UTHETA**2, TKE*1000/UTHETA**2. Y,U/UTHETA,U1/UTHETA, 4E13.6 RECORDS 3-4 MINIMUM V/UTHETA,V1/UTHETA, 3E13.6 VALUES -U1V1*1000/UTHETA**2, TKE*1000/UTHETA**2. Y,U/UTHETA,U1/UTHETA, 7I6 RECORDS 5-18 V/UTHETA,V1/UTHETA, NORMALIZED VALUES -U1V1*1000/UTHETA**2, X/C = 0.938 TKE*1000/UTHETA**2 11 18 Y,U/UTHETA,U1/UTHETA, 4E13.6 RECORDS 1-2 MAXIMUM V/UTHETA,V1/UTHETA, 3E13.6 VALUES -U1V1*1000/UTHETA**2, TKE*1000/UTHETA**2. Y,U/UTHETA,U1/UTHETA, 4E13.6 RECORDS 3-4 MINIMUM V/UTHETA,V1/UTHETA, 3E13.6 VALUES -U1V1*1000/UTHETA**2, TKE*1000/UTHETA**2. Y,U/UTHETA,U1/UTHETA, 7I6 RECORDS 5-18 V/UTHETA,V1/UTHETA, NORMALIZED VALUES -U1V1*1000/UTHETA**2, X/C = 1.000 TKE*1000/UTHETA**2 12 16 Y,U/UTHETA,U1/UTHETA, 4E13.6 RECORDS 1-2 MAXIMUM V/UTHETA,V1/UTHETA, 3E13.6 VALUES -U1V1*1000/UTHETA**2, TKE*1000/UTHETA**2. Y,U/UTHETA,U1/UTHETA, 4E13.6 RECORDS 3-4 MINIMUM V/UTHETA,V1/UTHETA, 3E13.6 VALUES -U1V1*1000/UTHETA**2, TKE*1000/UTHETA**2. Y,U/UTHETA,U1/UTHETA, 7I6 RECORDS 5-16 V/UTHETA,V1/UTHETA, NORMALIZED VALUES -U1V1*1000/UTHETA**2, X/C = 1.125 TKE*1000/UTHETA**2 13 19 Y,U/UTHETA,U1/UTHETA, 4E13.6 RECORDS 1-2 MAXIMUM V/UTHETA,V1/UTHETA, 3E13.6 VALUES -U1V1*1000/UTHETA**2, TKE*1000/UTHETA**2. Y,U/UTHETA,U1/UTHETA, 4E13.6 RECORDS 3-4 MINIMUM V/UTHETA,V1/UTHETA, 3E13.6 VALUES -U1V1*1000/UTHETA**2, TKE*1000/UTHETA**2. Y,U/UTHETA,U1/UTHETA, 7I6 RECORDS 5-19 V/UTHETA,V1/UTHETA, NORMALIZED VALUES -U1V1*1000/UTHETA**2, X/C = 1.250 TKE*1000/UTHETA**2 14 19 Y,U/UTHETA,U1/UTHETA, 4E13.6 RECORDS 1-2 MAXIMUM V/UTHETA,V1/UTHETA, 3E13.6 VALUES -U1V1*1000/UTHETA**2, TKE*1000/UTHETA**2. Y,U/UTHETA,U1/UTHETA, 4E13.6 RECORDS 3-4 MINIMUM V/UTHETA,V1/UTHETA, 3E13.6 VALUES -U1V1*1000/UTHETA**2, TKE*1000/UTHETA**2. Y,U/UTHETA,U1/UTHETA, 7I6 RECORDS 5-19 V/UTHETA,V1/UTHETA, NORMALIZED VALUES -U1V1*1000/UTHETA**2, X/C = 1.375 TKE*1000/UTHETA**2 A SAMPLE PROGRAM FOR READING FILE 2 AND PRINTING IS SHOWN BELOW. THE JCL IS FOR THE STANFORD CIT FACILITY. CHECK WITH YOUR OWN COMPUTER FACILITY FOR THE EXACT JCL NEEDED //TAPE JOB BRC$NJ /*SETUP TAPE=1, INPUT=(LIBRARY NUMBER ASSIGNED TO TAPE) //EXEC FORTCG //FORT.SYSIN DO * C PROGRAM TO READ FILE 3 OFF THE TAPE AND C PRINT THE MAXIMA AND MINIMA ON ALL THE VARIABLES REAL X/C(33), PTOT(33) READ (23,30) X/CMX,PTOTMX READ (23,30) X/CMN,PTOTMN C SET N =THE NUMBER OF RECORDS IN THE FILE MINUS 2 N=35-2 DO 10 I=1,N 10 READ (23,40) X/C(I), PTOT(I) WRITE (6,50) X/CMX,PTOTMX WRITE (6,50) X/CMN,PTOTMN DO 20 I=1,N 20 WRITE(6,60) X/C(I),PTOT(I) 30 FORMAT(2E13.6) 40 FORMAT(2E13.6) 50 FORMAT(2X,2E13.6) STOP END //GO.FT23F001 DD UNIT=T1600,VOL=SER=(TAPE LIBRARY NUMBER), // DISP=(OLD,KEEP),DCB=(RECFM=FB, LREC=80, BLOCKSIZE=8000,DEN=3) // LABEL =(2,NL) -------------- END OF FILE NUMBER 1062------------- ----------------- FILE NUMBER 1063----------------- 0.161880E 01 0.660600E 00 0.500000E 00 0.355300E 00 0 1923 280 1422 559 704 838 406 1117 0 1397 3049 1676 4916 1956 5693 2235 6390 2514 6721 2793 7042 3073 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