NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Some historical trends in the research and development of aircraftA survey of some trends in aircraft design was made in an effort to determine the relation between research, development, test, and evaluation (RDT and E) and aircraft mission capability, requirements, and objectives. Driving forces in the history of aircraft include the quest for speed which involved design concepts incorporating jet propulsion systems and low drag features. The study of high speed design concepts promoted new experimental and analytical research techniques. These research techniques, in turn, have lead to concepts offering new performance potential. Design trends were directed toward increased speed, efficiency, productivity, and safety. Generally speaking, the research and development effort has been evolutionary in nature and, with the exception of the transition to supersonic flight, little has occurred since the origin of flight that has drastically changed the basic design fundamentals of aircraft. However, this does not preclude the possibility of dramatic changes in the future since the products of research are frequently unpredictable. Advances should be expected and sought in improved aerodynamics (reduced drag, enhanced lift, flow field exploitation); propulsion (improved engine cycles, multimode engines, alternate fuels, alternate power sources); structures (new materials, manufacturing techniques); all with a view toward increased efficiency and utility.
Document ID
19830018514
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Spearman, M. L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
April 1, 1983
Subject Category
Aeronautics (General)
Report/Patent Number
NAS 1.15:84665
NASA-TM-84665
Report Number: NAS 1.15:84665
Report Number: NASA-TM-84665
Accession Number
83N26785
Funding Number(s)
PROJECT: RTOP 505-43-43-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available