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Technical Paper

Large Eddy Breakup Devices as Low Reynolds Number Airfoils

1986-10-01
861769
LEBU drag reduction is shown to be an extremely sensitive function of device micro-geometry at the low Reynolds numbers of all current investigations, and by analogy with conventional low-Reynolds number airfoil testing, the conclusion is drawn that the full potential for LEBU drag reduction must be explored at chord Reynolds numbers of 300,000 and above.
Event

Attend - Innovations in Mobility: Aerospace Digital Summit

2024-06-23
Innovations in Mobility: Aerospace Digital Summitaerospace mobility leaders convene leverage cutting-edge technology, design, develop safety measures, integrate current regulations, suggest future policies, expand markets, diversify revenue streams.
Standard

Fuse, Current Limiter Type, Aircraft

2023-03-27
CURRENT
AS5372A
This specification covers the requirements for current limiter type fuses for use in aircraft primary electrical power systems conforming to MIL-STD-704.
Technical Paper

Detached Eddy Simulation on a Swept Hybrid Model in the IRT

2015-06-15
2015-01-2122
As they can be useful in robustly and accurately predicting large separation regions and capturing flow unsteadiness, a Detached Eddy Simulation (DES) approach has been adopted for simulating the flow over these large high-lift wing sections.
Technical Paper

Spacelab ECLS Current Status

1982-02-01
820884
This paper describes the major ECLS functions with particular respect to the current Flight Unit hardware status. It also includes recent design modifications, improvements, and adaptations resulting from Spacelab qualification and integration.
Technical Paper

Current Problems in Airline Engines

1935-01-01
350083
AN outline of some current problems in aircraft engines with particular reference to the types used for main-line scheduled-transport operations is presented, it being limited so far as possible to a consideration of the conventional four-stroke gasoline-engine.
Standard

Document for 270 Voltage Direct Current (270 V DC) System

2017-11-30
CURRENT
ARP4729A
This SAE Aerospace Recommended Practice (ARP) provides technical design and application information related to the generation, distribution, control, and utilization of aircraft 270 V DC electrical power systems and support equipment. This document also provides references and definitions to permit comparisons of various electrical systems and components.
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