package MH.JavaFoil;
//Localized.java
import java.util.ListResourceBundle;
/** This class contains all the localized strings of JavaFoil.
*
* The strings are stored in a table of String Objects.
* Each entry consists of a pair of Strings:
*
* - the FIRST one is a key and must never be changed,
* - the SECOND one is the string to be used for display.
*
*
* This sample file contains the default strings in English.
* These are used, when no localized version is found.
*
* To create a localized version:
*
* -
* translate the SECOND entry of each pair in the contents Object.
*
* -
* if you have the JDK and want to test your translation:
*
* -
* rename the class to Localized_XX, where XX is the international
* language code (e.g. "en" for "En"glish)
*
* -
* rename the file from Localized.java, to Localized_XX.java,
* where XX is again the language code of choice
*
* -
* translate with "javac" to produce the class file Localized_XX.class
*
* -
* add the class file to javafoil.jar using "jar"
*
* -
* define LocalizationCheck=1 on the command line to produce a list of
* keywords found (or nmissing)
*
*
*
*
*
* Mail the translated file to: Martin.Hepperle@dlr.de
*
*
Initially Created: April 2001
*
Initial Author: Martin Hepperle
*
* Currently (2006) the following translations are embedded into JavaFoil:
*
*
* | English | April 2001 | Martin Hepperle | Germany |
*
* | German | April 2001 | Martin Hepperle | Germany |
*
* | French | March 2001 | Giorgio Toso | Canada |
*
* | Italian | September 2001 | Giorgio Toso | Canada |
*
* | Spanish | January 2003 | Israel Gandara | Spain |
*
* | Portuguese(european) | October 2003 | João Alveirnho Correia | Portugal |
*
* | Finnish | March 2005 | Matti Hyötyniemi | Finland |
*
* | Dutch | March 2008 | Henri Rommelse | Netherlands |
*
*
*/
public class Localized_pt
extends ListResourceBundle
{
/** This method returns an array of String Objects containing
* the keys and the localized strings.
*/
public Object[][] getContents()
{
return contents;
}
/** The array of key-value pairs
*/
static final Object[][] contents =
{ // localize the SECOND entry of each pair (first one is a lookup key)
// --- details for this translation ----
{"LOCALIZED_LANG", "European Portugese"}, // the language of this file
{"LOCALIZED_AUTHOR", "João Alveirnho"}, // the translator of this file
{"LOCALIZED_DATE", "October 2003"}, // the date of this translation
{"LOCALIZED_EMAIL", "?@?"}, // the eMail of the translator
// --- the application specific strings start here ----
{"APPLOAD", "Carregando o Applet"},
{"GEOMETRY", "Geometria"}, // tab caption
{"MODIFY", "Modificar"}, // tab caption
{"DESIGN", "Desenho"}, // tab caption
{"VELOCITY", "Velocidade"}, // tab caption
{"FIELD", "Flowfield"}, // tab caption
{"BLAYER", "Sub Camada"}, // tab caption
{"POLAR", "Polar"}, // tab caption
/*NEW*/{"AIRCRAFT", "Aircraft"}, // tab caption
{"OPTIONS", "Opções"}, // tab caption
{"READY", "Pronto"}, // status line message
{"NAME", "Nome"},
{"ADDPLTS", "Adicionar aos gráficos"}, // checkbox
{"SAVE", "Gravar..."}, // button caption
{"OPEN", "Abrir..."}, // button caption
{"PRINT", "Imprimir..."}, // button caption
{"COPYTEXT", "Copiar (Texto)"}, // button caption
{"COPYHTML", "Copiar (HTML)"}, // button caption
{"PASTETEXT", "Colar (Text)"}, // button caption
{"OKAY", "Ok"}, // button in message box
{"SAVESETTINGS", "Guardar Configuração"}, // dialog box caption
{"OPENSETTINGS", "Abrir Configurações"}, // dialog box caption
{"SAVEAIRFOIL", "Guardar Coordenadas do Perfil"}, // dialog box caption
{"OPENAIRFOIL", "Abrir Coordenadas do Perfil"}, // dialog box caption
{"SAVESCRIPT", "Guardar Script"}, // dialog box caption
{"OPENSCRIPT", "Abrir Script"}, // dialog box caption
{"SAVEPOLARS", "Guardar Polares"}, // dialog box caption
{"SAVEFIELD", "Guardar Dados Campo"}, // dialog box caption
{"STAT_SAVE", "Guardando..."}, // status bar message
{"STAT_WORK", "A processar..."}, // status bar message
{"STAT_STRM", "linhas de Fluxo..."}, // status bar message
/*NEW*/{"INFO_CAPTION", "JavaFoil - Information"}, // caption for message boxes
{"WRN_CAPTION", "JavaFoil - Aviso"}, // caption for message boxes
{"ERR_CAPTION", "JavaFoil - Erro"}, // caption for message boxes
{"ERR_WRITE", "Erro ao escrever o ficheiro."}, // error message
{"ERR_READ", "Erro ao ler o ficheiro."}, // error message
{"ERR_FILE", "Ficheiro não encontrado."}, // error message
{"ERR_DECIMAL",
"não foram encontrados numeros de virgula flutuante no input.\n" +
"por favor verifique as configurações do Javafoil!\n" +
"tentando reparar- possivel substituição de caracteres decimais por"}, // error message
{"EXPIRED", "A sua cópia do JavaFoil tem mais de 6 meses.\n" +
"Devia procurar na web uma versão mais recente.\n" +
"http://www.mh-aerotools.de/"},
// general items
{"XC", "x/c"}, // normalized x-coordinate
{"YC", "y/c"}, // normalized y-coordinate
{"XS", "x/s"}, // arc-length-coordinate
{"LD", "L/D"}, // glide ratio L/D
{"AC", "A.C."}, // "aerodynamic center", "neutral point"
/*NEW*/{"CP", "C.P."}, // "center of pressure"
{"DELTA", "delta"}, // thickness delta_1, _2, _3
{"BLSHAPE", "H"}, // shape parameter H_12, H_32
{"MACH_NO", "Mach"}, // Mach Number
{"ASPECT_RATIO", "Alongamento"}, // Aspect Ratio == (span^2/Area)
{"WIG_LONG", "Efeito de solo"}, // used in the status line to say "airfoil in ground effect"
{"WIG_ABBREV", "WIG"}, // used in legend to abbreviate "airfoil in ground effect"
/*NEW*/{"FROUDE_LONG", "Froude effect"}, // used in the status line to say "airfoil in Froude effect"
/*NEW*/{"FROUDE_ABBREV", "FR"}, // used in legend to abbreviate "airfoil in Froude effect"
/*NEW*/{"SUM", "Sum"},
/*NEW*/{"SHOWDIST", "Show distributions of"},
// *** Geometry card
{"GEOMTITLE", "Geometria do perfil"},
{"COORDS", "Coordenadas"},
{"CLEAR", "Limpar"}, // button caption
{"UPDATEVW", "Actualizar a vista"},
{"NACATITLE", "Criar um Perfil NACA"},
{"NACATYPE", "Familia"}, // caption for choice
{"P_NACA_4", "NACA 4-digitos(e.g. 2412)"}, // choice
{"P_NACA_4M", "NACA 4-digitos, modified (e.g. 0012-74)"}, // choice
{"P_NACA_5", "NACA 5-digitos (normal e.g. 23012)"}, // choice
{"P_NACA_5M", "NACA 5-digitos (reflexed e.g. 23112)"}, // choice
{"P_NACA_6", "NACA 6-digitos (e.g. 64012)"}, // choice
{"P_NACA_16", "NACA 16-série (e.g. 16-412)"}, // choice
/*NEW*/{"P_TSAGI_B", "TsAGI \"B\" série"}, // choice
/*NEW*/{"P_NPL_EQH", "NPL EQH série"}, // choice
/*NEW*/{"P_BICONVEX", "biconvex airfoil"}, // choice
/*NEW*/{"P_WEDGE", "Wedge"}, // choice
/*NEW*/{"P_PLATE", "Cambered Plate"}, // choice
/*NEW*/{"P_VDVOOREN", "Van de Vooren symmetrical airfoil"}, // choice, a Van de Vooren conformal mapping airfoil
/*NEW*/{"P_NEWMAN", "Newman circular nose airfoil"}, // choice
/*NEW*/{"P_JOUKOVSKY", "Joukovsky airfoil"}, // choice
/*NEW*/{"P_HBK", "Helmbold-Keune airfoil"}, // choice, an airfoil according to Helmbold and Keune
{"POINTCOUNT", "Numero de pontos"},
{"THK", "espessura máx t/c"},
{"XTHK", "localização espessura máx xt/c"},
{"RLE1", "Raio Bordo de ataque"},
{"RLE2", "(4-digitos: 1.1019*(t/c)²)"},
/*NEW*/{"TEA", "Trailing Edge Angle"},
{"CAM", "Curvatura f/c"},
{"XCAM", "Curvatura(localização) xf/c"},
{"CLDES", "Desenho Coeficiente de Sustentação Cl"},
{"AMOD", "A-modificação"},
{"CLOSED_TE", "Modificar Secção NACA p/ Bordo de fuga Fechado"},
{"SHAPE", "Forma do Perfil"},
{"C_NACA4", "Este é um Perfil de uso geral"},
{"C_NACA4M", "isto é uma modificação da série de 4-digitos"},
{"C_NACA5", "momento inferior à série de 4-digitos"},
{"C_NACA6", "arrasto inferior à série de 4-digitos"},
{"C_NACA16", "esta série é usualmente utilizada em hélices"},
/*NEW*/{"C_TSAGIB", "This series had been developed at the TsAGI"}, // comment
/*NEW*/{"C_NPL_EQH", "British laminar flow sections (NPL EQH)"}, // comment
/*NEW*/{"C_CIRCARC",
"For supersonic flow, JavaFoil analysis not applicable"}, // comment
/*NEW*/{"C_WEDGE", "For supersonic flow, JavaFoil analysis not applicable"}, // comment
/*NEW*/{"C_PLATE", "Uses NACA 4-series camber line"}, // comment
/*NEW*/{"C_VDVOOREN", "Van de Vooren conformal mapping airfoil"}, // comment
/*NEW*/{"C_NEWMAN", "Composed of a circular nose and straight lines."}, // comment
/*NEW*/{"C_JOUKOVSKY","Created by conformal mapping"}, // comment
{"REM1", "p/ análise posterior o use bordo de fuga fechado."},
{"CREATE", "Criar Perfil"},
// *** Modify card
{"MODTITLE", "Modificar Perfil"}, // caption
{"SCALE", "Aumentar em"}, // label for scaling factor
{"FLAPCHORD", "Flap Corda xf/c"}, // label for flap chord length
{"FLAPANGLE", "Flap Deflecção"}, // label for deflection angle
{"ELEMENT", "Elemento"}, // label for element number
{"PIV_X", "eixo x"}, // label for pivot point x
{"PIV_Y", "eixo y"}, // label for pivot point y
{"ROT", "Rodar"}, // abel for rotation angle
{"TRANS_X", "Translação x"}, // label for translation in x direction
{"TRANS_Y", "translação y"}, // label for translation in y direction
{"TE_GAP", "Espaçamento do Bordo de ataque"}, // label for trailing edge thickness
{"REM2", "espessura e Curvatura só funcionam na direcção y."},
{"UNDO", "desfazer"},
{"EMPTY", " - vazio - "},
{"DUPLICATE", "duplicado"},
{"DELETE", "apagar"},
/*NEW*/{"FLIP", "Flip Y"}, // mirror along x-axis (+y -> -y)
// *** Design card
{"DESTITLE", "desenhar Perfil"}, // caption
{"RELAX", "Relax by"}, // label for relaxation factor
{"D_STEPS", "numero de passos"}, // label for number of design steps
{"D_STEP", "passo"}, // for step no. in status line
{"CP_SHORT", "Cp"}, // Pressure Coefficient, short
{"CP_LONG", "Coeficiente Pressão"}, // Pressure Coefficient, long
{"REM6", "desenho move as coordeadas só na direcção y."},
{"TARGET", "Alvo"}, // short label for plot legend
{"CURRENT", "currente"}, // short label for plot legend
{"NOSYMMETRY", "single side Cp-modification"},
{"SYMMETRY", "Modificar Cp Simétrico"},
{"ASYMMETRY", "anti-symmetric Cp-modification (camber)"},
{"SMOOTH", "Suaviza Cp Alvo"}, // use shape function to smooth target Cp
{"X_OR_S", "y(x) ou y(s)"}, // Cp versus x or versus arc length?
/*NEW*/{"LE_ZOOM", "LE Enlargement"}, // enlargement of leading edge region
{"SETUP", "Configuração"},
{"DODESIGN", "executar!"},
{"REDRAW", "Redesenhar"},
/*NEW*/{"DETAILS", "Details..."}, // button caption
// *** Velocity card
{"VELOTITLE", "distribuição de velocidades"}, // card caption, also on printout
{"ALFA_0", "1º Angulo de ataque"},
{"ALFA_1", "último Angulo"},
{"ALFA_D", "incremento Angulo"},
{"VELDIST", "distribuição de velocidades"},
/*NEW*/{"CPDIST", "Pressure Coefficient Distributions"},
/*NEW*/{"MACHDIST", "Mach Number Distributions"},
/*NEW*/{"VELRATIO", "Velocity Ratio v/V"},
/*NEW*/{"CPCOEFF", "Pressure Coefficient Cp"},
{"REM3",
"a distribuição de velocidades pode ser util para suavizar o perfil."},
{"CP_CRIT", "Cp*"}, // minimum local Cp value on surface of airfoil
{"MACH_CRIT", "M cr."}, // critical Mach Number = M at which locally supersonic flow occurs
{"ANALYZE", "Analiza-o!"},
// *** Flowfield card
{"FIELDTITLE", "Fluxo"}, // card caption, also on printout
{"X_STEPS", "passos na direcção X"}, // number of steps
{"Y_STEPS", "passos na direcção Y"}, // number of steps
{"TUFTS", "Tufos Pretos"}, // black velocity vectors
{"FIELDPLOT", "Campo colorido"}, // filled field "panels"
{"ISOLINES", "Isolinhas Cp"}, // white iso-Cp lines
{"NORMVECTOR", "Cp Vectores"}, // Cp vectors normal to surface
{"STREAMLINES", "Linhas fluxo"}, // streamlines from left border
{"ACCURACY", "precisão aumentada"}, // higher order integration (Runge-Kutta O4)
{"TIMED", "Temporizada"}, // checkbox to activate timed dashes
{"ZOOMOUT", "Campo de fluxo"}, // 100%, 200%, ...
{"COLORMAP", "Color Map Type"}, // 1, 2, ...
// *** Polars card
{"POLARTITLE", "Polares Perfil"}, // card caption, also on printout
{"RE_0", "1º Número Reynolds"},
{"RE_1", "último Número de Reynolds"},
{"RE_D", "incremento Número de Re."},
{"ROUGHNESS", "Acabamento da Superficie"},
{"ROUGH_0", "Acabamento suave"},
{"ROUGH_1", "tecido Pintado"},
{"ROUGH_2", "Padrão NACA"},
{"ROUGH_3", "insectos e sujidade"},
{"STALLMODEL", "modelo de Perda"}, // the various stall models
{"SM_1", "Calcfoil"},
{"SM_2", "Eppler"},
{"SM_3", "nenhum"},
{"TRANSITIONMODEL", "modelo de transição"}, // the various transition models
{"TM_1", "Padrão Eppler"},
{"TM_2", "Eppler extendido"},
{"TM_3", "Michel 1"},
{"TM_4", "Michel 2"},
{"TM_5", "H12-Re(s)"}, // name, do not translate
{"TM_6", "Granville"}, // name, do not translate
{"TM_7", "Drela e^n approximation, Xfoil before 1991"}, // name, do not translate
{"TM_8", "Drela e^n approximation, Xfoil after 1991"}, // name, do not translate
{"TM_9", "Arnal, approximation by Würz"}, // name, do not translate
{"DRAGPLOT", "Cl-Cd Gráfico"},
{"DRAGTABLE", "Cl-Cd Tabela"},
{"RE", "Re"}, // legend abbreviation for Reynolds number
{"CL", "Cl"}, // axis label lift coefficient
{"CM", "Cm 0.25"}, // axis label moment coefficient
{"CD", "Cd"}, // axis label drag coefficient
{"VV", "v/V"}, // axis label velocity ratio
{"REM4", "Um máximo de "}, // continued with a number and the REM5 string
{"REM5", "numeros de Reynolds são guardados nas tabelas."},
{"LIFT", "sustentação"}, // tab button caption, short for Lift coefficient vs. angle of attack
{"MOMENT", "Momento"}, // tab button caption, short for Moment coefficient vs. angle of attack
{"UPPER", "Superior"}, // tab button caption, short for upper surface (transition and separation)
{"LOWER", "Inferior"}, // tab button caption, short for lower surface (transition and separation)
{"UP_SUR", "extradorso"}, // caption for printout of polars
{"LO_SUR", "intradorso"}, // caption for printout of polars
{"TRANS", "transição"}, // caption for printout of polars
// error messages
{"ERR_ALFAS", "O angulo de ataque que escolheu cria um conjunto de dados muito grande.\n \nResetting to default"},
{"ERR_RENOS", "O número de Reynolds que escolheu cria um conjunto de dados muito grande.\n \nResetting to default"},
{"ERR_NOPOL", "Não há Polares para copiar ou gravar."},
{"ERR_NOFOIL", "Não há Perfil para analisar.\n Criar ou importar utilizando o Cartão da Geometria."},
{"ERR_HITGND",
"Pare: O Bordo de Ataque do Perfil\nIntersectaria o Solo."}, // used in message box for wing in ground effect
{"ERR_MATH", "Pare: Um erro matemático ocorreu.\nVerifique a geometria do perfile todos os parâmetros."},
// *** Aircraft card
/*NEW*/{"AIRCRAFTTITLE", "Flugzeug orientierte Polaren"}, // card caption, also on printout
/*NEW*/{"MS_0", "erste Flächenbelastung"}, // wing loading
/*NEW*/{"MS_1", "letzte Flächenbelastung"},
/*NEW*/{"MS_D", "Flächenbelastungsschritt"},
/*NEW*/{"CHORD", "Profiltiefe"}, // label for reference chord length
/*NEW*/{"M_OVER_S", "m/S"}, // formula
/*NEW*/{"WL", "Flächenbelastung"}, // textual form
// *** Options card
{"OC_TITLE", "Ajuste a(s) opção(ões) necessária(s)."}, // card caption
{"VERSION", "Versão"}, // JavaFoil Version x.yy
{"COUNTRYSETTINGS", "Configurações de País"},
{"SYSSET", "As suas configurações de Sistema"},
{"USERNAME", "o seu nome é"},
{"OSNAME", "você está a correr"},
{"JAVANAME", "versão Java "},
{"JAVAMEMORY", "a memória Java é"},
{"KBYTES", "kB"},
{"LANGCODE", "Sistema: Código de linguagem é"},
{"COUNTRY", "país escolhido é"},
{"LANGUAGE", "lingua selecionada é"},
{"SYSACCESSDENIED", "impossivel aceder ao sistema.Propriedades, Provavelmente porque está a correr como applet"},
{"DECCHAR", "Caracter decimal"},
{"PATHSEP", "Separador de Path"},
{"DENSITY", "Densidade"},
{"KINVISC", "Viscosidade cinemática"},
{"VELSOUND", "Velocidade do Som"},
{"WIG_CB", "Efeito de solo(Solo a y=0)"}, // used for checkbox to say "ground at y=0 active"
/*NEW*/{"FREE_CB", "unbounded flow field"}, // used for checkbox to say "free flow field"
/*NEW*/{"FROUDE_CB", "Froude effect (free surface at y=0)"}, // used for checkbox to say "free surfec at y=0 active"
{"TRANSLAT_1", "tradução para"}, // first part of "Translation to ...language... by ...Name ..."
{"TRANSLAT_2", "por"}, // second part of "Translation to ...language... by ...Name ..."
/*NEW*/{"TRANSLAT_3", "There is no version of JavaFoil matching Your country settings."}, // message
/*NEW*/{"TRANSLAT_4", "If you like, You can create and send my your translation."}, // message
/*NEW*/{"TRANSLAT_5", "For details look into the folder 'Translation' in the installation directory."}, // message
{"ENGLISH", "Inglês"}, // English
{"GERMAN", "Alemão"}, // German
{"FRENCH", "Francês"}, // French
{"ITALIAN", "Italiano"}, // Italian
{"SPANISH", "Castelhano"}, // Spanish
{"PORTUGUESE", "Português"}, // Portuguese
{"DUTCH", "Holandês"}, // Dutch
{"FINNISH", "Suomi"}, // Finnish
/*NEW*/{"CHARSET","Character Set"},
/*NEW*/{"ENCODING", "used for files and clipboard exchange"},
// *** Boundary Layer card
{"BLTITLE", "Parametros da Sub camada laminar"}, // card caption, also on printout
{"ALFA", "Angulo de ataque"}, // label caption
{"DELTAPLOT", "Espessura do gráfico"}, // tab button caption
{"SHAPEPLOT", "Forma do Gráfico"}, // tab button caption
{"CFPLOT", "Cf do Gráfico"}, // tab button caption
{"TU", "T.S."}, // short label: transition upper
{"TL", "T.I."}, // short label: transition lower
{"SU", "S.S."}, // short label: separation upper
{"SL", "S.I."}, // short label: separation lower
{"BLSTATE", "Estado"}, // flow state: laminar or turbulent
{"LAM", "lam."}, // abbreviation: laminar
{"TUR", "turb."}, // abbreviation: turbulent
{"SEP", "sep."}, // abbreviation: separated
// *** Script frame
{"REC_START", "Iniciar Gravador"},
{"REC_STOP", "Parar Gravador"},
{"REC_RUN", "correr"},
{"REC_STEP", "incremento"},
{"SCRIPT", "Script"},
{"REM_SCR", "Comentário as linhas devem começar com//"},
{"REC_DATE", "Gravado em"}, // used to build a comment line like
{"REC_TIME", "às"}, // "recorded on 00/00/00 at 00:00:00 by ..."
{"REC_BY", "por"}, // (only if user name is accessible)
{"ERR_SCRIPT", "Erro no Script no comando"}, // used to build message "Script error in command '...'"
{"ERR_PARSE1", "Falta de parenteses fechados"}, //
{"ERR_PARSE2", "Comando desconhecido"}, //
{"ROW_SHORT", "R"}, // Row nnn in status bar of script editor
{"COL_SHORT", "C"}, // Col nnn in status bar of script editor
{"ROW_LONG", "linha"}, // Row nnn in error messages
{"COL_LONG", "Coluna"}, // Column nnn in error messages
};
}