Accession Number:

ADA110686

Title:

Supersonic Cruise/Transonic Maneuver Wing Section Development Study.

Descriptive Note:

Final rept. Aug 77-Nov 79,

Corporate Author:

ROCKWELL INTERNATIONAL EL SEGUNDO CA NORTH AMERICAN AIRCRAFT DIV

Personal Author(s):

Report Date:

1980-06-01

Pagination or Media Count:

77.0

Abstract:

Computational aerodynamic design of advanced fighter wings with well-controlled transonic maneuver flow and high supersonic cruise efficiency is described. Author

Subject Categories:

  • Attack and Fighter Aircraft
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE