Publication Date:
2019-07-13
Description:
An investigation of the vibration, performance, flutter, and forced response of the large-scale propfan, SR7L, and its aeroelastic model, SR7A, has been performed by applying available structural and aeroelastic analytical codes and then correlating measured and calculated results. Finite element models of the blades were used to obtain modal frequencies, displacements, stresses and strains. These values were then used in conjunction with a 3-D, unsteady, lifting surface aerodynamic theory for the subsequent aeroelastic analyses of the blades. The agreement between measured and calculated frequencies and mode shapes for both models is very good. Calculated power coefficients correlate well with those measured for low advance ratios. Flutter results show that both propfans are stable at their respective design points. There is also good agreement between calculated and measured blade vibratory strains due to excitation resulting from yawed flow for the SR7A propfan. The similarity of structural and aeroelastic results show that the SR7A propfan simulates the SR7L characteristics.
Keywords:
AIRCRAFT PROPULSION AND POWER
Type:
NASA-TM-101322
,
E-4260
,
NAS 1.15:101322
,
AIAA PAPER 88-3155
,
Joint Propulsion Conference; Jul 11, 1988 - Jul 13, 1988; Boston, MA; United States
Format:
application/pdf
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