ex6.out

Digital DATCOM Source Code and Examples

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  ****************************************************
  *    USAF STABILITY AND CONTROL  DIGITAL DATCOM    *
  *    PROGRAM REV. JAN 96   DIRECT INQUIRIES TO:    *
  *    WRIGHT LABORATORY  (WL/FIGC)  ATTN: W. BLAKE  *
  *      WRIGHT PATTERSON AFB, OHIO  45433           *
  *    PHONE [phone],   FAX [phone]    *
  ****************************************************
 Preparing to start the big loop
 At 1000
1                         CONERR - INPUT ERROR CHECKING
0 ERROR CODES - N* DENOTES THE NUMBER OF OCCURENCES OF EACH ERROR
0 A - UNKNOWN VARIABLE NAME
0 B - MISSING EQUAL SIGN FOLLOWING VARIABLE NAME
0 C - NON-ARRAY VARIABLE HAS AN ARRAY ELEMENT DESIGNATION - (N)
0 D - NON-ARRAY VARIABLE HAS MULTIPLE VALUES ASSIGNED
0 E - ASSIGNED VALUES EXCEED ARRAY DIMENSION
0 F - SYNTAX ERROR

0******************************  INPUT DATA CARDS  ******************************

  $FLTCON  NALPHA=9.0, ALSCHD=-2.0,0.0,2.0,4.0,8.0,12.0,16.0,20.0,24.0$          
  $FLTCON  NMACH=1.0, MACH(1)=0.6, RNNUB(1)=4.26E6$                              
  $OPTINS SREF=2.25, CBARR=0.822, BLREF=3.00$                                    
  $SYNTHS XCG=2.60, ZCG=0.0, XW=1.70, ZW=0.0, ALIW=0.0$                          
  $BODY NX=10.0,BNOSE=2.0,BTAIL=1.0,BLN=1.46,BLA=1.97,                           
    X(1)=0.0, .175,.322,.530,.850,1.46,2.5,3.43,3.97,4.57,                       
    R(1)=0.0, .0417,.0833,.125,.1665,.208,.208,.208,.178,.138$                   
  $WGPLNF CHRDTP=0.346,SSPNE=1.29,SSPN=1.5,CHRDR=1.16,SAVSI=45.0,CHSTAT=0.25,    
   SWAFP=0.0,TWISTA=0.0,SSPNDD=0.0,DHDADI=0.0,DHDADO=0.0,TYPE=1.0$               
  $WGSCHR TOVC=.06,DELTAY=1.3,XOVC=0.4,CLI=0.0,ALPHAI=0.0,CLALPA(1)=0.131,       
   CLMAX(1)=.82,CMO=0.0,LERI=.0025,CLAMO=.105$                                   
  $WGSCHR  CLMAXL=0.8, TCEFF=.03$                                                
  $ASYFLP NDELTA=5.0, DELTAL(1)=5.,10.,20.,30.,40.,                              
                      DELTAR(1)=-2.,-5.,-10.,-15.,-20.,                          
          STYPE=4.0, CHRDFI=.1116, CHRDFO=.0692,                                 
          SPANFI=1.109, SPANFO=1.5, PHETE=.0522$                                 
 CASEID PLAIN FLAP AILERON, EXAMPLE PROBLEM 6, CASE 1                            
 SAVE                                                                            
 NEXT CASE                                                                       
  $ASYFLP STYPE=3.0, DELTAD(1)=.0130,.0261,.0380,.0513,.0630,.0750,              
    DELTAS(1)=.013, .0261, .030, .0513, .0630, .0750,                            
    XSOC(1)=.6900,.6955,.6680,.6438,.6454,.6259,                                 
    XSPRME=0.55,                                                                 
    XSOC(1)=0.0357,0.0710,0.0956,0.1102,0.1365,0.1359$                           
 CASEID SPOILER-SLOT-DEFLECTOR ON WING, EXAMPLE PROBLEM 6, CASE 2                
 NEXT CASE                                                                       
1          THE FOLLOWING IS A LIST OF ALL INPUT CARDS FOR THIS CASE.
0
  $FLTCON  NALPHA=9.0, ALSCHD=-2.0,0.0,2.0,4.0,8.0,12.0,16.0,20.0,24.0$          
  $FLTCON  NMACH=1.0, MACH(1)=0.6, RNNUB(1)=4.26E6$                              
  $OPTINS SREF=2.25, CBARR=0.822, BLREF=3.00$                                    
  $SYNTHS XCG=2.60, ZCG=0.0, XW=1.70, ZW=0.0, ALIW=0.0$                          
  $BODY NX=10.0,BNOSE=2.0,BTAIL=1.0,BLN=1.46,BLA=1.97,                           
    X(1)=0.0, .175,.322,.530,.850,1.46,2.5,3.43,3.97,4.57,                       
    R(1)=0.0, .0417,.0833,.125,.1665,.208,.208,.208,.178,.138$                   
  $WGPLNF CHRDTP=0.346,SSPNE=1.29,SSPN=1.5,CHRDR=1.16,SAVSI=45.0,CHSTAT=0.25,    
   SWAFP=0.0,TWISTA=0.0,SSPNDD=0.0,DHDADI=0.0,DHDADO=0.0,TYPE=1.0$               
  $WGSCHR TOVC=.06,DELTAY=1.3,XOVC=0.4,CLI=0.0,ALPHAI=0.0,CLALPA(1)=0.131,       
   CLMAX(1)=.82,CMO=0.0,LERI=.0025,CLAMO=.105$                                   
  $WGSCHR  CLMAXL=0.8, TCEFF=.03$                                                
  $ASYFLP NDELTA=5.0, DELTAL(1)=5.,10.,20.,30.,40.,                              
                      DELTAR(1)=-2.,-5.,-10.,-15.,-20.,                          
          STYPE=4.0, CHRDFI=.1116, CHRDFO=.0692,                                 
          SPANFI=1.109, SPANFO=1.5, PHETE=.0522$                                 
 CASEID PLAIN FLAP AILERON, EXAMPLE PROBLEM 6, CASE 1                            
 SAVE                                                                            
 NEXT CASE                                                                       
0 INPUT DIMENSIONS ARE IN FT, SCALE FACTOR IS 1.0000

 Return to main program from M01O01
 Return to main program from M50O62
 Return to main program from M02O02
 Return to main program from M51O63
1                               AUTOMATED STABILITY AND CONTROL METHODS PER APRIL 1976 VERSION OF DATCOM
                                         CHARACTERISTICS AT ANGLE OF ATTACK AND IN SIDESLIP
                                                       WING-BODY CONFIGURATION
                                           PLAIN FLAP AILERON, EXAMPLE PROBLEM 6, CASE 1
 
 -----------------------  FLIGHT CONDITIONS  ------------------------           --------------  REFERENCE DIMENSIONS  ------------
  MACH    ALTITUDE   VELOCITY    PRESSURE    TEMPERATURE     REYNOLDS             REF.      REFERENCE LENGTH   MOMENT REF. CENTER
 NUMBER                                                       NUMBER              AREA       LONG.     LAT.     HORIZ      VERT
             FT       FT/SEC     LB/FT**2       DEG R         1/FT               FT**2        FT        FT        FT        FT
0 0.600                                                    4.2600E+06             2.250      0.822     3.000     2.600     0.000
0                                                               -------------------DERIVATIVE (PER DEGREE)-------------------
0 ALPHA     CD       CL       CM       CN       CA       XCP        CLA          CMA          CYB          CNB          CLB
0