500 lines
24 KiB
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500 lines
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<a href="#pub-methods">Public Member Functions</a> |
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<a href="classAirframe-members.html">List of all members</a> </div>
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<div class="headertitle"><div class="title">Airframe Class Reference</div></div>
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<p>Represents the structural body and aerodynamic shell of a rocket stage.
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<a href="#details">More...</a></p>
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<p><code>#include <<a class="el" href="Airframe_8h_source.html">Airframe.h</a>></code></p>
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<table class="memberdecls">
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<tr class="heading"><td colspan="2"><h2 class="groupheader"><a id="pub-methods" name="pub-methods"></a>
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Public Member Functions</h2></td></tr>
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<tr class="memitem:a123b40dd9395cc05a7a89a5a3004298c" id="r_a123b40dd9395cc05a7a89a5a3004298c"><td class="memItemLeft" align="right" valign="top"> </td><td class="memItemRight" valign="bottom"><a class="el" href="#a123b40dd9395cc05a7a89a5a3004298c">Airframe</a> (const std::string &name, double length, double diameter, double dryMass, double dragCoefficient)</td></tr>
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<tr class="memdesc:a123b40dd9395cc05a7a89a5a3004298c"><td class="mdescLeft"> </td><td class="mdescRight">Constructs a new <a class="el" href="classAirframe.html" title="Represents the structural body and aerodynamic shell of a rocket stage.">Airframe</a>. <br /></td></tr>
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<tr class="separator:a123b40dd9395cc05a7a89a5a3004298c"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:ae0ee4e8d348c4527494482f361c6fb6d" id="r_ae0ee4e8d348c4527494482f361c6fb6d"><td class="memItemLeft" align="right" valign="top"> </td><td class="memItemRight" valign="bottom"><a class="el" href="#ae0ee4e8d348c4527494482f361c6fb6d">~Airframe</a> ()=default</td></tr>
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<tr class="memdesc:ae0ee4e8d348c4527494482f361c6fb6d"><td class="mdescLeft"> </td><td class="mdescRight">Default destructor. <br /></td></tr>
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<tr class="separator:ae0ee4e8d348c4527494482f361c6fb6d"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:afcc955b8abdf1403030238ca2648b5d7" id="r_afcc955b8abdf1403030238ca2648b5d7"><td class="memItemLeft" align="right" valign="top">double </td><td class="memItemRight" valign="bottom"><a class="el" href="#afcc955b8abdf1403030238ca2648b5d7">getLength</a> () const</td></tr>
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<tr class="memdesc:afcc955b8abdf1403030238ca2648b5d7"><td class="mdescLeft"> </td><td class="mdescRight">Gets the total length of the airframe. <br /></td></tr>
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<tr class="separator:afcc955b8abdf1403030238ca2648b5d7"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:a012eb2b1e8f32065ecf39c2aeefc649e" id="r_a012eb2b1e8f32065ecf39c2aeefc649e"><td class="memItemLeft" align="right" valign="top">double </td><td class="memItemRight" valign="bottom"><a class="el" href="#a012eb2b1e8f32065ecf39c2aeefc649e">getDiameter</a> () const</td></tr>
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<tr class="memdesc:a012eb2b1e8f32065ecf39c2aeefc649e"><td class="mdescLeft"> </td><td class="mdescRight">Gets the maximum diameter of the airframe. <br /></td></tr>
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<tr class="separator:a012eb2b1e8f32065ecf39c2aeefc649e"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:a17109f526af0c620af27b8c446677c7d" id="r_a17109f526af0c620af27b8c446677c7d"><td class="memItemLeft" align="right" valign="top">double </td><td class="memItemRight" valign="bottom"><a class="el" href="#a17109f526af0c620af27b8c446677c7d">getDryMass</a> () const</td></tr>
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<tr class="memdesc:a17109f526af0c620af27b8c446677c7d"><td class="mdescLeft"> </td><td class="mdescRight">Gets the dry mass of the airframe. <br /></td></tr>
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<tr class="separator:a17109f526af0c620af27b8c446677c7d"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:ab5efbcf7355c8968f74cf63d38820581" id="r_ab5efbcf7355c8968f74cf63d38820581"><td class="memItemLeft" align="right" valign="top">double </td><td class="memItemRight" valign="bottom"><a class="el" href="#ab5efbcf7355c8968f74cf63d38820581">getDragCoefficient</a> () const</td></tr>
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<tr class="memdesc:ab5efbcf7355c8968f74cf63d38820581"><td class="mdescLeft"> </td><td class="mdescRight">Gets the aerodynamic drag coefficient. <br /></td></tr>
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<tr class="separator:ab5efbcf7355c8968f74cf63d38820581"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:a72ccd7f9f379776d9f893712fe8ce17d" id="r_a72ccd7f9f379776d9f893712fe8ce17d"><td class="memItemLeft" align="right" valign="top">double </td><td class="memItemRight" valign="bottom"><a class="el" href="#a72ccd7f9f379776d9f893712fe8ce17d">getReferenceArea</a> () const</td></tr>
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<tr class="memdesc:a72ccd7f9f379776d9f893712fe8ce17d"><td class="mdescLeft"> </td><td class="mdescRight">Calculates the reference area for drag computation. <br /></td></tr>
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<tr class="separator:a72ccd7f9f379776d9f893712fe8ce17d"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:a51b1712adfba0528bb3efa275984da5e" id="r_a51b1712adfba0528bb3efa275984da5e"><td class="memItemLeft" align="right" valign="top">const std::string & </td><td class="memItemRight" valign="bottom"><a class="el" href="#a51b1712adfba0528bb3efa275984da5e">getName</a> () const</td></tr>
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<tr class="memdesc:a51b1712adfba0528bb3efa275984da5e"><td class="mdescLeft"> </td><td class="mdescRight">Gets the name of the airframe. <br /></td></tr>
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<tr class="separator:a51b1712adfba0528bb3efa275984da5e"><td class="memSeparator" colspan="2"> </td></tr>
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</table><table class="memberdecls">
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<tr class="heading"><td colspan="2"><h2 class="groupheader"><a id="pri-attribs" name="pri-attribs"></a>
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Private Attributes</h2></td></tr>
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<tr class="memitem:a291492dddc479251ea1953b0ed299eca" id="r_a291492dddc479251ea1953b0ed299eca"><td class="memItemLeft" align="right" valign="top">std::string </td><td class="memItemRight" valign="bottom"><a class="el" href="#a291492dddc479251ea1953b0ed299eca">name_</a></td></tr>
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<tr class="memdesc:a291492dddc479251ea1953b0ed299eca"><td class="mdescLeft"> </td><td class="mdescRight">Name of the airframe. <br /></td></tr>
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<tr class="separator:a291492dddc479251ea1953b0ed299eca"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:a5c5f193c1bd7b92c9dc6692baced7200" id="r_a5c5f193c1bd7b92c9dc6692baced7200"><td class="memItemLeft" align="right" valign="top">double </td><td class="memItemRight" valign="bottom"><a class="el" href="#a5c5f193c1bd7b92c9dc6692baced7200">length_</a></td></tr>
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<tr class="memdesc:a5c5f193c1bd7b92c9dc6692baced7200"><td class="mdescLeft"> </td><td class="mdescRight">Total length [m]. <br /></td></tr>
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<tr class="separator:a5c5f193c1bd7b92c9dc6692baced7200"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:af123137166b93f18c0423c2bddc8da55" id="r_af123137166b93f18c0423c2bddc8da55"><td class="memItemLeft" align="right" valign="top">double </td><td class="memItemRight" valign="bottom"><a class="el" href="#af123137166b93f18c0423c2bddc8da55">diameter_</a></td></tr>
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<tr class="memdesc:af123137166b93f18c0423c2bddc8da55"><td class="mdescLeft"> </td><td class="mdescRight">Maximum diameter [m]. <br /></td></tr>
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<tr class="separator:af123137166b93f18c0423c2bddc8da55"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:abe76be70e49f5da0715a326b33eb4d5f" id="r_abe76be70e49f5da0715a326b33eb4d5f"><td class="memItemLeft" align="right" valign="top">double </td><td class="memItemRight" valign="bottom"><a class="el" href="#abe76be70e49f5da0715a326b33eb4d5f">dryMass_</a></td></tr>
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<tr class="memdesc:abe76be70e49f5da0715a326b33eb4d5f"><td class="mdescLeft"> </td><td class="mdescRight">Structural dry mass [kg]. <br /></td></tr>
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<tr class="separator:abe76be70e49f5da0715a326b33eb4d5f"><td class="memSeparator" colspan="2"> </td></tr>
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<tr class="memitem:a0d5040caae7f9b6ac1854b614b8b6f2c" id="r_a0d5040caae7f9b6ac1854b614b8b6f2c"><td class="memItemLeft" align="right" valign="top">double </td><td class="memItemRight" valign="bottom"><a class="el" href="#a0d5040caae7f9b6ac1854b614b8b6f2c">dragCoefficient_</a></td></tr>
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<tr class="memdesc:a0d5040caae7f9b6ac1854b614b8b6f2c"><td class="mdescLeft"> </td><td class="mdescRight">Drag coefficient (Cd). <br /></td></tr>
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<tr class="separator:a0d5040caae7f9b6ac1854b614b8b6f2c"><td class="memSeparator" colspan="2"> </td></tr>
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</table>
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<a name="details" id="details"></a><h2 class="groupheader">Detailed Description</h2>
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<div class="textblock"><p>Represents the structural body and aerodynamic shell of a rocket stage. </p>
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<p>The <a class="el" href="classAirframe.html" title="Represents the structural body and aerodynamic shell of a rocket stage.">Airframe</a> class manages geometric dimensions, mass properties, and aerodynamic characteristics needed for simulation. </p>
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</div><h2 class="groupheader">Constructor & Destructor Documentation</h2>
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<a id="a123b40dd9395cc05a7a89a5a3004298c" name="a123b40dd9395cc05a7a89a5a3004298c"></a>
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<h2 class="memtitle"><span class="permalink"><a href="#a123b40dd9395cc05a7a89a5a3004298c">◆ </a></span>Airframe()</h2>
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<td class="memname">Airframe::Airframe </td>
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<td>(</td>
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<td class="paramtype">const std::string &</td> <td class="paramname"><span class="paramname"><em>name</em></span>, </td>
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<td class="paramtype">double</td> <td class="paramname"><span class="paramname"><em>length</em></span>, </td>
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<td class="paramtype">double</td> <td class="paramname"><span class="paramname"><em>diameter</em></span>, </td>
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<td class="paramkey"></td>
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<td></td>
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<td class="paramtype">double</td> <td class="paramname"><span class="paramname"><em>dryMass</em></span>, </td>
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<td class="paramtype">double</td> <td class="paramname"><span class="paramname"><em>dragCoefficient</em></span> )</td>
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<p>Constructs a new <a class="el" href="classAirframe.html" title="Represents the structural body and aerodynamic shell of a rocket stage.">Airframe</a>. </p>
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<dl class="params"><dt>Parameters</dt><dd>
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<table class="params">
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<tr><td class="paramname">name</td><td>Name of the airframe component. </td></tr>
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<tr><td class="paramname">length</td><td>Total length of the airframe (meters). </td></tr>
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<tr><td class="paramname">diameter</td><td>Maximum body diameter (meters). </td></tr>
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<tr><td class="paramname">dryMass</td><td>Dry mass of the airframe structure (kilograms). </td></tr>
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<tr><td class="paramname">dragCoefficient</td><td>Estimated drag coefficient (unitless). </td></tr>
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</table>
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</dd>
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<h2 class="memtitle"><span class="permalink"><a href="#ae0ee4e8d348c4527494482f361c6fb6d">◆ </a></span>~Airframe()</h2>
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<td class="memname">Airframe::~Airframe </td>
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<td>(</td>
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<td class="paramname"><span class="paramname"><em></em></span></td><td>)</td>
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<td></td>
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<span class="mlabels"><span class="mlabel default">default</span></span> </td>
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<p>Default destructor. </p>
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<h2 class="groupheader">Member Function Documentation</h2>
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<a id="a012eb2b1e8f32065ecf39c2aeefc649e" name="a012eb2b1e8f32065ecf39c2aeefc649e"></a>
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<h2 class="memtitle"><span class="permalink"><a href="#a012eb2b1e8f32065ecf39c2aeefc649e">◆ </a></span>getDiameter()</h2>
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<td class="memname">double Airframe::getDiameter </td>
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<td>(</td>
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<td class="paramname"><span class="paramname"><em></em></span></td><td>)</td>
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<td> const</td>
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<p>Gets the maximum diameter of the airframe. </p>
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<dl class="section return"><dt>Returns</dt><dd>Diameter in meters. </dd></dl>
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<a id="ab5efbcf7355c8968f74cf63d38820581" name="ab5efbcf7355c8968f74cf63d38820581"></a>
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<h2 class="memtitle"><span class="permalink"><a href="#ab5efbcf7355c8968f74cf63d38820581">◆ </a></span>getDragCoefficient()</h2>
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<td class="memname">double Airframe::getDragCoefficient </td>
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<td>(</td>
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<p>Gets the aerodynamic drag coefficient. </p>
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<dl class="section return"><dt>Returns</dt><dd>Drag coefficient (dimensionless). </dd></dl>
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<h2 class="memtitle"><span class="permalink"><a href="#a17109f526af0c620af27b8c446677c7d">◆ </a></span>getDryMass()</h2>
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<td class="memname">double Airframe::getDryMass </td>
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<td>(</td>
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<td class="paramname"><span class="paramname"><em></em></span></td><td>)</td>
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<p>Gets the dry mass of the airframe. </p>
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<dl class="section return"><dt>Returns</dt><dd>Mass in kilograms. </dd></dl>
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<h2 class="memtitle"><span class="permalink"><a href="#afcc955b8abdf1403030238ca2648b5d7">◆ </a></span>getLength()</h2>
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<td class="memname">double Airframe::getLength </td>
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<td>(</td>
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<p>Gets the total length of the airframe. </p>
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<dl class="section return"><dt>Returns</dt><dd>Length in meters. </dd></dl>
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<a id="a51b1712adfba0528bb3efa275984da5e" name="a51b1712adfba0528bb3efa275984da5e"></a>
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<h2 class="memtitle"><span class="permalink"><a href="#a51b1712adfba0528bb3efa275984da5e">◆ </a></span>getName()</h2>
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<td class="memname">const std::string & Airframe::getName </td>
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<td>(</td>
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<p>Gets the name of the airframe. </p>
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<dl class="section return"><dt>Returns</dt><dd>Name as a constant reference. </dd></dl>
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<a id="a72ccd7f9f379776d9f893712fe8ce17d" name="a72ccd7f9f379776d9f893712fe8ce17d"></a>
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<h2 class="memtitle"><span class="permalink"><a href="#a72ccd7f9f379776d9f893712fe8ce17d">◆ </a></span>getReferenceArea()</h2>
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<td class="memname">double Airframe::getReferenceArea </td>
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<td>(</td>
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<p>Calculates the reference area for drag computation. </p>
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<p>Reference area = Pi * (diameter / 2)^2</p>
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<dl class="section return"><dt>Returns</dt><dd>Cross-sectional area in square meters. </dd></dl>
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<h2 class="groupheader">Member Data Documentation</h2>
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<a id="af123137166b93f18c0423c2bddc8da55" name="af123137166b93f18c0423c2bddc8da55"></a>
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<h2 class="memtitle"><span class="permalink"><a href="#af123137166b93f18c0423c2bddc8da55">◆ </a></span>diameter_</h2>
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<td class="memname">double Airframe::diameter_</td>
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<span class="mlabels"><span class="mlabel private">private</span></span> </td>
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<p>Maximum diameter [m]. </p>
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<a id="a0d5040caae7f9b6ac1854b614b8b6f2c" name="a0d5040caae7f9b6ac1854b614b8b6f2c"></a>
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<h2 class="memtitle"><span class="permalink"><a href="#a0d5040caae7f9b6ac1854b614b8b6f2c">◆ </a></span>dragCoefficient_</h2>
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<span class="mlabels"><span class="mlabel private">private</span></span> </td>
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<p>Drag coefficient (Cd). </p>
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<a id="abe76be70e49f5da0715a326b33eb4d5f" name="abe76be70e49f5da0715a326b33eb4d5f"></a>
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<h2 class="memtitle"><span class="permalink"><a href="#abe76be70e49f5da0715a326b33eb4d5f">◆ </a></span>dryMass_</h2>
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<p>Structural dry mass [kg]. </p>
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<a id="a5c5f193c1bd7b92c9dc6692baced7200" name="a5c5f193c1bd7b92c9dc6692baced7200"></a>
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<h2 class="memtitle"><span class="permalink"><a href="#a5c5f193c1bd7b92c9dc6692baced7200">◆ </a></span>length_</h2>
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<p>Total length [m]. </p>
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<a id="a291492dddc479251ea1953b0ed299eca" name="a291492dddc479251ea1953b0ed299eca"></a>
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<h2 class="memtitle"><span class="permalink"><a href="#a291492dddc479251ea1953b0ed299eca">◆ </a></span>name_</h2>
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<span class="mlabels"><span class="mlabel private">private</span></span> </td>
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<p>Name of the airframe. </p>
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<hr/>The documentation for this class was generated from the following files:<ul>
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<li>include/<a class="el" href="Airframe_8h_source.html">Airframe.h</a></li>
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<li>src/<a class="el" href="Airframe_8cpp.html">Airframe.cpp</a></li>
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