{"push_id":946691113,"size":1,"distinct_size":1,"ref":"refs/heads/master","head":"599e76c77f6ac58b94035f7b3cdf3e3bfb2cc958","before":"b8efe8a118c99715cf33c0840bd005acfbd320ee","commits":[{"sha":"599e76c77f6ac58b94035f7b3cdf3e3bfb2cc958","author":{"email":"c03e147483aaf80db76fe90ccc7b52cdcca638a1@aol.com","name":"ManuRuocco"},"message":" Minor changes in mi SandBox. Now it is possible to evaluate CL of a wing having alpha body as input","distinct":true,"url":"https://api.github.com/repos/Aircraft-Design-UniNa/jpad/commits/599e76c77f6ac58b94035f7b3cdf3e3bfb2cc958"}]}