CONFIG LIB 1.5
Configuration Files Library (by TGG 2020)
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panukl_prj.h
1/*********************************************************************/
2/* */
3/* Config files library - (C) TGG 2015 */
4/* */
5/*********************************************************************/
6/* Warszawa, 2015 */
7/*********************************************************************/
8/* */
9/* File: panukl_prj.h */
10/* */
11/* Author: T.Grabowski */
12/* */
13/* Contents - prj file data (SDSA creation) class */
14/* */
15/* */
16/*********************************************************************/
17/* */
18/* */
19
20#ifndef _PANUKL_PRJ_H_
21#define _PANUKL_PRJ_H_
22
23#include "iofun.h"
24
26
27class PANUKL_PRJ : public IOFUN
28{
29 public:
30
31 char SDSA_dir[256];
32 int iH;
33 int iL;
34 int iV;
35
36 double dAlfa0;
37 double dAlfak;
38 double dAlf;
39 double dBeta;
40 double dP;
41 double dQ;
42 double dR;
43 double dMa0;
44 double dMak;
45 double dMa;
46 double dH;
47 double dL;
48 double dV;
49
50 double dCfe;
51 double dAoA_max;
52
53 char DAT_file[256];
54 char DAT_file1[256];
55 char DAT_file2[256];
56 char DAT_file3[256];
57
58 int iCompress;
59 int iMaxProc;
60 int iProc;
61
62 int iNum1;
63 int iNum2;
64 int iMeth;
65 int iAngle;
66 int iPitchX;
67
68 double dXNum1;
69 double dXNum2;
70
71 PANUKL_PRJ( void );
72 ~PANUKL_PRJ( void );
73
75 void Clean();
77 int Read( char *PrjFile );
79 int Write( char *PrjFile );
80};
81
82#endif /*_PANUKL_PRJ_H_*/
IOFUN
Simple I/O functions class.
Definition iofun.h:42
PANUKL_PRJ
Parameters file for PanProject program - creates data set for SDSA.
Definition panukl_prj.h:28
PANUKL_PRJ::iNum2
int iNum2
number of the last panel taken for global coefficients calculation
Definition panukl_prj.h:63
PANUKL_PRJ::dAlfa0
double dAlfa0
left (lower) bound of angle of attack [deg]
Definition panukl_prj.h:36
PANUKL_PRJ::dV
double dV
rudder deflection corresponding to mesh from DAT_file3 [deg]
Definition panukl_prj.h:48
PANUKL_PRJ::SDSA_dir
char SDSA_dir[256]
path name for output - aerodynamic data files set for SDSA
Definition panukl_prj.h:31
PANUKL_PRJ::DAT_file1
char DAT_file1[256]
data (mesh+wake) file [.DAT] elevator deflected
Definition panukl_prj.h:54
PANUKL_PRJ::iCompress
int iCompress
compressibility flag (0-none, 1-Prandtl-Galuert, 2-Karman-Tsien, 3-direct)
Definition panukl_prj.h:58
PANUKL_PRJ::dAlf
double dAlf
step of angle of attack [deg]
Definition panukl_prj.h:38
PANUKL_PRJ::DAT_file3
char DAT_file3[256]
data (mesh+wake) file [.DAT] rudder deflected
Definition panukl_prj.h:56
PANUKL_PRJ::iMaxProc
int iMaxProc
max number of parallel process (shouldn't be greater than real number of CPUs (cores)
Definition panukl_prj.h:59
PANUKL_PRJ::dH
double dH
elevator deflection corresponding to mesh from DAT_file1 [deg]
Definition panukl_prj.h:46
PANUKL_PRJ::iPitchX
int iPitchX
flag to take X component of forces for pitching moment calculation(0/1)
Definition panukl_prj.h:66
PANUKL_PRJ::iH
int iH
flag to compute configuration with elevator deflected (0/1)
Definition panukl_prj.h:32
PANUKL_PRJ::dBeta
double dBeta
sideslip angle [deg]
Definition panukl_prj.h:39
PANUKL_PRJ::dMak
double dMak
right (upper) bound of Mach number range
Definition panukl_prj.h:44
PANUKL_PRJ::dL
double dL
aileron deflection corresponding to mesh from DAT_file2 [deg]
Definition panukl_prj.h:47
PANUKL_PRJ::dXNum2
double dXNum2
upper bound of range of X coordinate taken for global coefficients calculation
Definition panukl_prj.h:69
PANUKL_PRJ::iProc
int iProc
current number of CPUs (cores) - set by program
Definition panukl_prj.h:60
PANUKL_PRJ::dP
double dP
roll rate [rad/s]
Definition panukl_prj.h:40
PANUKL_PRJ::iMeth
int iMeth
number of differentiation method (see PANUKL manual)
Definition panukl_prj.h:64
PANUKL_PRJ::dR
double dR
yaw rate [rad/s]
Definition panukl_prj.h:42
PANUKL_PRJ::dAlfak
double dAlfak
right (upper) bound of angle of attack [deg]
Definition panukl_prj.h:37
PANUKL_PRJ::dMa0
double dMa0
left (lower) bound of Mach number range
Definition panukl_prj.h:43
PANUKL_PRJ::Clean
void Clean()
cleans local variables
Definition panukl_prj.cpp:26
PANUKL_PRJ::DAT_file2
char DAT_file2[256]
data (mesh+wake) file [.DAT] aileron deflected
Definition panukl_prj.h:55
PANUKL_PRJ::iV
int iV
flag to compute configuration with rudder deflected (0/1)
Definition panukl_prj.h:34
PANUKL_PRJ::Write
int Write(char *PrjFile)
writes the [.prj] file
Definition panukl_prj.cpp:104
PANUKL_PRJ::dAoA_max
double dAoA_max
max. value of angle of attack [deg]
Definition panukl_prj.h:51
PANUKL_PRJ::DAT_file
char DAT_file[256]
data (mesh+wake) file [.DAT] for basic configuration
Definition panukl_prj.h:53
PANUKL_PRJ::dCfe
double dCfe
parasite drag coefficient
Definition panukl_prj.h:50
PANUKL_PRJ::dMa
double dMa
step of Mach number
Definition panukl_prj.h:45
PANUKL_PRJ::dXNum1
double dXNum1
lower bound of range of X coordinate taken for global coefficients calculation
Definition panukl_prj.h:68
PANUKL_PRJ::iAngle
int iAngle
averaging flag (0/1)
Definition panukl_prj.h:65
PANUKL_PRJ::iL
int iL
flag to compute configuration with aileron deflected (0/1)
Definition panukl_prj.h:33
PANUKL_PRJ::iNum1
int iNum1
number of the first panel taken for global coefficients calculation
Definition panukl_prj.h:62
PANUKL_PRJ::Read
int Read(char *PrjFile)
reads the [.prj] file
Definition panukl_prj.cpp:52
PANUKL_PRJ::dQ
double dQ
pitch rate [rad/s]
Definition panukl_prj.h:41
iofun.h
This file contains some smart I/O functions.