Hypothetically, if aerodynamicists had the opportunity to somehow raise the speed of sound in air to an infinite level so that air was no longer compressed, how would this affect aircraft related aerodynamics? Are there cases a higher speed of sound would be helpful rather than a hindrance?
Would subsonic aircraft designs be able to fly much faster without design changes?
Would we be able to design axial compressors with much higher pressure ratios per stage?
Perhaps much higher thrust could be generated from the same size propeller?
Are there cases where this would not be desirable? Such as spacecraft re-entry for instance?