APPLICATION OF LAMINAR FLOW CONTROL TECHNOLOGY TO OPTIMUM SUPERSONIC CRUISE.

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Abstract:

No Abstract Identified

Author(s):
No Author(s) Identified
Author Organization(s):
NORTHROP CORP HAWTHORNE CA NORAIR DIV
Descriptive Note:
Bi-monthly progress rept. no. 9, 15 Feb-15 Apr 65.
Pagination:
0021

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
NOR-65-93
Contract/Grant Number(s):
AF 33(657)-11618
Project Number(s):
AF-136612
 Subject Terms
Communities of Interest:
No COI(s) Identified
Descriptor(s):
*LAMINAR FLOW, *SWEPTBACK WINGS, SUPERSONIC AIRCRAFT, BOUNDARY LAYER CONTROL, AREA SUCTION, TRAILING EDGES, LAMINAR BOUNDARY LAYER, COMPRESSIBLE FLOW, PERTURBATION THEORY
Field(s)/Group(s):
Aircraft, Fluid Mechanics
Keyword(s):
LAMINAR FLOW CONTROL
Report Date:
1965 Apr 01