Pressure Distributions on a Delta Wing - Horizontal Stabilizer Combination at Mach Numbers from 0.3 to 2.9. Volume 8. Wing Chordwise Pressure Distributions, Effect of: Nacelles, Flaps, Spoilers, Sideslip, and Reynolds Number. Part 2.

Document Details

Document Type
Technical Report
Publication Date
Jul 15, 1972
Accession Number
AD0903837

Entities

People

  • James D. Knittel
  • Johan P. Moulijn
  • Marjorie E. Manro

Organizations

  • Boeing

Tags

DTIC Thesaurus Topics

  • Airfoils
  • Delta Wings
  • Horizontal Stabilizers
  • Mach Number
  • Pressure Distribution
  • Reynolds Number
  • Sideslip
  • Stabilization Systems