NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Supersonic aerodynamics of delta wingsThrough the empirical correlation of experimental data and theoretical analysis, a set of graphs has been developed which summarize the inviscid aerodynamics of delta wings at supersonic speeds. The various graphs which detail the aerodynamic performance of delta wings at both zero-lift and lifting conditions were then employed to define a preliminary wing design approach in which both the low-lift and high-lift design criteria were combined to define a feasible design space.
Document ID
19880008231
Document Type
Technical Publication (TP)
Authors
Wood, Richard M. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1988
Subject Category
AERODYNAMICS
Report/Patent Number
NASA-TP-2771
NAS 1.60:2771
L-16212
Funding Number(s)
PROJECT: RTOP 505-61-71-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

NameType 19880008231.pdf STI