The first JetStar leading edge flight test was made November 30, 1983. The JetStar was flown for more than 3 years. The titanium leading edge test articles today remain in virtually the same condition as they were in on that first flight. No degradation of laminar flow performance has occurred as a result of service. The JetStar simulated airline service flights have demonstrated that effective, practical leading edge systems are available for future commercial transports. Specific conclusions based on the results of the simulated airline service test program are summarized
A study was conducted to evaluate alternatives in the design of laminar flow control (LFC) subsonic ...
A flight-test campaign of a supersonic natural laminar flow airfoil has been recently completed. The...
An investigation of leading edge contamination by insects was conducted with a JetStar airplane inst...
The overall objective of the flight tests on the JetStar aircraft was to demonstrate the effectivene...
NASA's program for development of a laminar flow technology base for application to commercial trans...
Achieving laminar flow on the wings of a commercial transport involves difficult problems associated...
The effectiveness and practicality of candidate leading edge systems for suction laminar flow contro...
Under the Aircraft Energy Efficiency - Laminar Flow Control Program, there are currently three fligh...
The flight testing conducted over the past 10 years in the NASA laminar-flow control (LFC) will be r...
A flight experiment, conducted at NASA Dryden Flight Research Center, investigated the effects of su...
A review of natural laminar flow (NLF) flight experiences over the period from the 1930's to the pre...
An F-104G aircraft at NASA's Dryden Flight Research Center has been equipped with a specially design...
Considerable progress has been made in the development of laminar flow technology for commercial tra...
The potential of natural laminar flow for significant drag reduction and improved efficiency for air...
The NASA Leading-Edge Flight Test (LEFT) program addressed the environmental issues which were poten...
A study was conducted to evaluate alternatives in the design of laminar flow control (LFC) subsonic ...
A flight-test campaign of a supersonic natural laminar flow airfoil has been recently completed. The...
An investigation of leading edge contamination by insects was conducted with a JetStar airplane inst...
The overall objective of the flight tests on the JetStar aircraft was to demonstrate the effectivene...
NASA's program for development of a laminar flow technology base for application to commercial trans...
Achieving laminar flow on the wings of a commercial transport involves difficult problems associated...
The effectiveness and practicality of candidate leading edge systems for suction laminar flow contro...
Under the Aircraft Energy Efficiency - Laminar Flow Control Program, there are currently three fligh...
The flight testing conducted over the past 10 years in the NASA laminar-flow control (LFC) will be r...
A flight experiment, conducted at NASA Dryden Flight Research Center, investigated the effects of su...
A review of natural laminar flow (NLF) flight experiences over the period from the 1930's to the pre...
An F-104G aircraft at NASA's Dryden Flight Research Center has been equipped with a specially design...
Considerable progress has been made in the development of laminar flow technology for commercial tra...
The potential of natural laminar flow for significant drag reduction and improved efficiency for air...
The NASA Leading-Edge Flight Test (LEFT) program addressed the environmental issues which were poten...
A study was conducted to evaluate alternatives in the design of laminar flow control (LFC) subsonic ...
A flight-test campaign of a supersonic natural laminar flow airfoil has been recently completed. The...
An investigation of leading edge contamination by insects was conducted with a JetStar airplane inst...