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MarAlderMarAlder
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add naca profiles
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‎schema/cpacs_schema.xsd‎

Lines changed: 87 additions & 2 deletions
Original file line numberDiff line numberDiff line change
@@ -4721,7 +4721,7 @@ cpacs@dlr.de
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<xsd:annotation>
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<xsd:documentation>Defines the number of control points that should be used for approximating the given points with a B-spline curve. The minimal value is 3.</xsd:documentation>
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</xsd:annotation>
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<xsd:complexType>
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<xsd:complexType>
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<xsd:simpleContent>
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<xsd:restriction base="integerBaseType">
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<xsd:minExclusive value="3"/>
@@ -4735,7 +4735,7 @@ cpacs@dlr.de
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The number of control points is increased automatically until the approximation error lies below the given maximum approximation error.
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</xsd:documentation>
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</xsd:annotation>
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<xsd:complexType>
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<xsd:complexType>
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<xsd:simpleContent>
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<xsd:restriction base="doubleBaseType">
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<xsd:minExclusive value="0"/>
@@ -26048,6 +26048,90 @@ The fuel tank volume type should also be used for the wing fuel tank</xsd:docume
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</xsd:complexContent>
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</xsd:complexType>
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<xsd:complexType name="nacaProfileType">
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<xsd:annotation>
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<xsd:appinfo>
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<sd:schemaDoc>
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<ddue:summary>
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<ddue:para>NACA airfoil definition</ddue:para>
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</ddue:summary>
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<ddue:remarks>
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<ddue:content>
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<ddue:para>Parametric definition of a NACA airfoil (4-digit or 5-digit series).</ddue:para>
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</ddue:content>
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</ddue:remarks>
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</sd:schemaDoc>
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</xsd:appinfo>
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</xsd:annotation>
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<xsd:complexContent>
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<xsd:extension base="complexBaseType">
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<xsd:sequence>
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<xsd:choice>
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<xsd:element name="naca4DigitCode">
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<xsd:annotation>
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<xsd:appinfo>
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<sd:schemaDoc>
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<ddue:summary>
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<ddue:para>NACA 4-digit airfoil code</ddue:para>
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</ddue:summary>
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<ddue:remarks>
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<ddue:para>Four digits defining a NACA 4-digit airfoil, e.g. <ddue:emphasis>2412</ddue:emphasis> or <ddue:emphasis>0012</ddue:emphasis>.</ddue:para>
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</ddue:remarks>
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</sd:schemaDoc>
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</xsd:appinfo>
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</xsd:annotation>
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<xsd:simpleType>
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<xsd:restriction base="xsd:token">
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<xsd:length value="4"/>
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<xsd:pattern value="[0-9]+"/>
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</xsd:restriction>
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</xsd:simpleType>
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</xsd:element>
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<xsd:element name="naca5DigitCode">
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<xsd:annotation>
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<xsd:appinfo>
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<sd:schemaDoc>
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<ddue:summary>
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<ddue:para>NACA 5-digit airfoil code</ddue:para>
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</ddue:summary>
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<ddue:remarks>
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<ddue:para>Five digits defining a NACA 5-digit airfoil, e.g. <ddue:emphasis>23012</ddue:emphasis>.</ddue:para>
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</ddue:remarks>
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</sd:schemaDoc>
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</xsd:appinfo>
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</xsd:annotation>
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<xsd:simpleType>
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<xsd:restriction base="xsd:token">
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<xsd:length value="5"/>
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<xsd:pattern value="[0-9]+"/>
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</xsd:restriction>
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</xsd:simpleType>
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</xsd:element>
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</xsd:choice>
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<xsd:element name="trailingEdgeThickness" minOccurs="0">
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<xsd:annotation>
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<xsd:appinfo>
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<sd:schemaDoc>
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<ddue:summary>
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<ddue:para>Trailing edge thickness</ddue:para>
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</ddue:summary>
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<ddue:remarks>
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<ddue:para>Trailing edge thickness normalized with respect to chord length. Must be greater than or equal to 0. A value of 0 corresponds to a closed trailing edge.</ddue:para>
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</ddue:remarks>
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</sd:schemaDoc>
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</xsd:appinfo>
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</xsd:annotation>
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<xsd:simpleType>
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<xsd:restriction base="xsd:double">
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<xsd:minInclusive value="0"/>
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</xsd:restriction>
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</xsd:simpleType>
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</xsd:element>
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</xsd:sequence>
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</xsd:extension>
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</xsd:complexContent>
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</xsd:complexType>
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<xsd:complexType name="nacelleCenterCowlType">
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<xsd:annotation>
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<xsd:appinfo>
@@ -29177,6 +29261,7 @@ The fuel tank volume type should also be used for the wing fuel tank</xsd:docume
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<xsd:element name="pointList" type="curvePointListXYZType"/>
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<xsd:element name="cst2D" type="cst2DType"/>
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<xsd:element name="standardProfile" type="standardProfileType"/>
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<xsd:element name="nacaProfile" type="nacaProfileType"/>
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</xsd:choice>
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</xsd:sequence>
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<xsd:attribute name="symmetry" type="symmetryXyXzYzType"/>

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