Assertion: airfoil's value | /r/HasProperty | given
Facets:
Source sentences:
text: a=1 is the default if no value is given.
text: a=1 is the default if no value is given.
text: If the value of C L {\displaystyle C_{L}} for a wing at a specified angle of attack is given, then the lift produced for specific flow conditions can be determined:
text: Typical values both for the range of deep stall, as defined above, and the locked-in trim point are given for the Douglas DC-9 Series 10 by Schaufele.