Results 91 to 100 of about 1,125 (144)

Multidisciplinary Conceptual Design for Reduced-Emission Rotorcraft [PDF]

open access: yes
Python-based wrappers for OpenMDAO are used to integrate disparate software for practical conceptual design of rotorcraft. The suite of tools which are connected thus far include aircraft sizing, comprehensive analysis, and parametric geometry. The tools
Johnson, Wayne   +2 more
core   +1 more source

Study of aircraft in intraurban transportation systems, volume 1 [PDF]

open access: yes
An analysis of an effective short range, high density computer transportation system for intraurban systems is presented. The seven county Detroit, Michigan, metropolitan area, was chosen as the scenario for the analysis.
Kesling, P. H.   +5 more
core   +1 more source

Aeronautical Engineering: A special bibliography with indexes, supplement 64, December 1975 [PDF]

open access: yes
This bibliography lists 288 reports, articles, and other documents introduced into the NASA scientific and technical information system in November ...

core   +1 more source

Study of research and development requirements of small gas-turbine combustors [PDF]

open access: yes
A survey is presented of the major small-engine manufacturers and governmental users. A consensus was undertaken regarding small-combustor requirements.
Demetri, E. P.   +2 more
core   +1 more source

High Speed Balancing Applied to the T700 Engine [PDF]

open access: yes
The work performed under Contracts NAS3-23929 and NAS3-24633 is presented. MTI evaluated the feasibility of high-speed balancing for both the T700 power turbine rotor and the compressor rotor.
Lee, C., Martin, M., Walton, J.
core   +1 more source

The cost of applying current helicopter external noise reduction methods while maintaining realistic vehicle performance [PDF]

open access: yes
Analytical methods were developed and/or adopted for calculating helicopter component noise, and these methods were incorporated into a unified total vehicle noise calculation model.
Bowes, M. A.
core   +1 more source

Compound cycle engine for helicopter application [PDF]

open access: yes
The Compound Cycle Engine (CCE) is a highly turbocharged, power compounded, ultra-high power density, light-weight diesel engine. The turbomachinery is similar to a moderate pressure ratio, free power turbine engine and the diesel core is high speed and ...
Castor, Jere G.
core   +1 more source

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