Accession Number:

ADA181217

Title:

Journal of China University of Science and Technology (Selected Articles),

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH

Personal Author(s):

Report Date:

1987-05-18

Pagination or Media Count:

34.0

Abstract:

Contents Effect of Nose Bluntness on Twin Wave Interference Application of Finite Element Method to Transonic Airfoils - A Preliminary Steady Subcritical Calculation. Chinese Translations China

Subject Categories:

  • Fluid Mechanics
  • Guided Missile Reentry Vehicles
  • Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE