Aerodynamic Studies of Wing Body Configurations with Moderate Aspect Ratio.

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Abstract:

The main objectives of the research were to carry out the theoretical analysis of the flow field near a wing body configuration, to develop the far field solutions and to study their interference effects on another airplane. Analyses have been carried out and definite results are obtained in the following topics 1 the motion and decay of vortex lines, 2 the connection of near field data to far field solution, 3 turbulent flow and boundary layer separation, and 4 the aerodynamic effects on an airplane by an incident shock. Author

Author(s):
Ferri, Antonio ; Ting, Lu
Author Organization(s):
NEW YORK UNIV BRONX SCHOOL OF ENGINEERING AND SCIENCE
Descriptive Note:
Final rept.,
Pagination:
0012

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
AROSR-TR-72-1020
Contract/Grant Number(s):
AF-AFOSR-1062-67
Task Number(s):
978201
Project Number(s):
AF-9782
Monitor Series:
TR-72-1020
 Subject Terms
Communities of Interest:
Air Platforms
Descriptor(s):
(*WING BODY CONFIGURATIONS, FLOW FIELDS), (*AVIATION SAFETY, SHOCK WAVES), VORTICES, DEGRADATION, BOUNDARY LAYER TRANSITION, FLOW SEPARATION, TURBULENCE, DUCTS
Field(s)/Group(s):
Aerodynamics, Terminal Flight Facilities, Fluid Mechanics
Keyword(s):
*TRAILING AIRCRAFT, TURBULENCE DECAY
Report Date:
1972 Feb 01