ASE 120K

Research on Forward Swept Wing Aircraft

Sukhoi 37, Berkut

by Mohit Garg

 

 

 

  1. Airflow at 0 degree Angle of Attack
  2. Airflow around Nose Landing Gear at 0 degree Angle of Attack
  3. Airflow around Nose Landing Gear at 7 degree Angle of Attack
  4. Wing Tip Vortex at 7 degree Angle of Attack
  5. Vertical Stabilizer Tip Vortex at 7 degree Angle of Attack
  6. Airflow around Leading Edge Strake at 7 degree Angle of Attack
  7. Airflow Separation over the Wing Surface at 7 degree Angle of Attack
  8. Wake Survey Behind the Model at 7 degree Angle of Attack
  9. Canard Tip Vortex Using Tuft at 7 degree Angle of Attack
  10. Vertical Stabilizer Tip Vortex Using Tuft at 7 degree Angle of Attack
  11. Airflow around Nose Landing Gear at 18 degree Angle of Attack (Also Notice the Vortex Behind the Cockpit)
  12. Wing Tip Vortex at 18 degree Angle of Attack
  13. Airflow around Leading Edge Strake at 18 degree Angle of Attack
  14. Canard Tip and Leading Edge Strake Vortex at 18 degree Angle of Attack
  15. Canard Tip Vortex Using Tuft at 18 degree Angle of Attack
  16. Vertical Stabilizer Tip Vortex Using Tuft at 18 degree Angle of Attack
  17. Wing Tip Vortex Using Tuft at 18 degree Angle of Attack
  18. Wing Root Vortex Using Tuft at 18 degree Angle of Attack
  19. Trailing Edge Strake Flap Tip Vortex Using Tuft at 18 degree Angle of Attack