Aircraft Design

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Across
  1. 4. FLIGHT AT SPEEDS GREATER THAN THE SPEED OF SOUND
  2. 7. IS A FIXED WING SECTION ATTACHED TO THE BACK OF THE FUSELAGE THAT PROVIDES STABILITY FOR THE AIRCRAFT AND HELPS IT TO FLY STRAIGHT.
  3. 8. IS THE LOCATION OF THE CENTER OF GRAVITY (CG) ON THE AIRCRAFT
  4. 13. IS THE UPPER ANGLE OF THE WINGS FROM THE WING ROOT TO THE TIPS.
  5. 15. THE POINT WHERE ALL OF THE AIRCRAFT’S WEIGHT IS CENTERED.
  6. 17. IS THE DISTANCE FROM THE DATUM LINE TO THE CENTER OF GRAVITY FOR A SPECIFIC ITEM.
  7. 20. FLIGHT AT SPEEDS JUST UNDER OR JUST ABOVE THE SPEED OF SOUND (700-780 MPH)
  8. 21. IS WHEN THE WEIGHT OF AN AIRCRAFT ACTS LIKE A PENDULUM AND SWINGS THE AIRCRAFT BACK INTO POSITION WHEN THE RELATIVE WIND DISTURBS LATERAL STABILITY.
  9. 23. THE HIGHEST LOAD FACTOR FOR WHICH STRUCTURAL PARTS ARE DESIGNED NOT TO FAIL
  10. 24. WHICH IS THE FORCE ON THE AIRCRAFT THAT DEFLECTS FROM FLIGHT AND PRODUCES STRESS ON THE AIRCRAFT.
  11. 25. WHICH IS THE TOTAL WEIGHT OF THE AIRPLANE DIVIDED BY THE AREA OF THE WINGS.
  12. 27. THE POINT WHERE UPWARD LIFT IS APPLIED TO THE WING.
  13. 28. IS THE COMPLETE CENTRAL STRUCTURE TO WHICH THE WING, TAIL SURFACES, AND ENGINES ARE ATTACHED ON AN AIRPLANE.
Down
  1. 1. OR CG RANGE,
  2. 2. IS WHEN THE LEADING EDGE OF THE WING IS SLOPED BACKWARD
  3. 3. ARE SMALL, MOVEABLE PIECES IN THE TOP, CENTER OF THE WING.
  4. 5. FLIGHT AT SPEEDS LESS THAN THE SPEED OF SOUND
  5. 6. IS A SMALL, MOVEABLE SECTION ATTACHED TO THE HORIZONTAL STABILIZER USING HINGES
  6. 9. IS THE UPWARD PORTION OF THE TAIL ON AN AIRCRAFT
  7. 10. WHICH IS THE LOAD IMPOSED BY FLIGHT MANEUVERS
  8. 11. WHICH IS THE WEIGHT OF THE AIRCRAFT ITSELF
  9. 12. IS THE WEIGHT OF THE AIRCRAFT MULTIPLIED BY THE ARM.
  10. 14. IS THE ABILITY OF AN AIRCRAFT TO INHERENTLY CORRECT DISTURBANCES TO ITS EQUILIBRIUM.
  11. 16. IS A SMALL, MOVEABLE SECTION ATTACHED TO THE VERTICAL STABILIZER USING HINGES.
  12. 18. IS AN IMAGINARY VERTICAL PLANE ON THE AIRCRAFT ESTABLISHED BY THE MANUFACTURER
  13. 19. WHICH IS THE AREA OF THE FUSELAGE WHERE THE RELATIVE WIND CAN AFFECT LATERAL STABILITY.
  14. 22. AIRCRAFT WHERE THE WINGS ARE MOUNTED ABOVE THE FUSELAGE.
  15. 26. ARE HINGED, MOVEABLE PIECES AT THE REAR OF EACH WING