COMPRCombustortypes:Can,Annular.BypassratioTransonicFlowIsentropicefficiencyγc =1.4*Callssomeoneby theircall sign*"The aircraftis just a rackto put theengine on""This is notan AE classor an aircraftanalysisclass"Cp =γ−1 γR *Shoutoutto Dr.Haven*SpankageHighPressureturbine"Back whenI did mydissertation""Beyondthe scopeof thisclass"*MentionsDiet Dr.Pepper*"Guys I'mnot gonnabe herenext week"Re=(ρ×v×L)/μ"Waitfor it"*Girl inthe reddressstory*"Backwhen Iwas inGE"GASTABBrynerNumberInlet machno. has tobe >1.0COMPRCombustortypes:Can,Annular.BypassratioTransonicFlowIsentropicefficiencyγc =1.4*Callssomeoneby theircall sign*"The aircraftis just a rackto put theengine on""This is notan AE classor an aircraftanalysisclass"Cp =γ−1 γR *Shoutoutto Dr.Haven*SpankageHighPressureturbine"Back whenI did mydissertation""Beyondthe scopeof thisclass"*MentionsDiet Dr.Pepper*"Guys I'mnot gonnabe herenext week"Re=(ρ×v×L)/μ"Waitfor it"*Girl inthe reddressstory*"Backwhen Iwas inGE"GASTABBrynerNumberInlet machno. has tobe >1.0

ME 417 Bingo! - Call List

(Print) Use this randomly generated list as your call list when playing the game. There is no need to say the BINGO column name. Place some kind of mark (like an X, a checkmark, a dot, tally mark, etc) on each cell as you announce it, to keep track. You can also cut out each item, place them in a bag and pull words from the bag.


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  1. COMPR
  2. Combustor types: Can, Annular.
  3. Bypass ratio
  4. Transonic Flow
  5. Isentropic efficiency
  6. γc = 1.4
  7. *Calls someone by their call sign*
  8. "The aircraft is just a rack to put the engine on"
  9. "This is not an AE class or an aircraft analysis class"
  10. Cp = γ−1 γR ​
  11. *Shoutout to Dr. Haven*
  12. Spankage
  13. High Pressure turbine
  14. "Back when I did my dissertation"
  15. "Beyond the scope of this class"
  16. *Mentions Diet Dr. Pepper*
  17. "Guys I'm not gonna be here next week"
  18. Re=(ρ×v×L)/μ
  19. "Wait for it"
  20. *Girl in the red dress story*
  21. "Back when I was in GE"
  22. GASTAB
  23. Bryner Number
  24. Inlet mach no. has to be >1.0