Calculation of lift and pitching moments due to angle of attack and steady pitching velocity at supersonic speeds for thin sweptback tapered wings with streamwise tips and supersonic leading and trailing edges

John C. Martin, Kenneth Margolis, Isabella Jeffreys
naca-tn-2699
Jun 1952


The results of the analysis are presented as a series of design charts. Some illustrative variations of the derivatives and of the chordwise center-of-pressure locations with the various wing design parameters are also include.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1952/naca-tn-2699.pdf