The NASA research program on propulsion for supersonic cruise aircraft [PDF]
The objectives and status of the propulsion portion of a program aimed at advancing the technology and establishing a data base appropriate for the possible future development of supersonic cruise aircraft are reviewed.
Weber, R. J.
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Recent Progress in Inkjet-Printed Thin-Film Transistors. [PDF]
Adv Sci (Weinh), 2019 Chung S, Cho K, Lee T.
europepmc +1 more source
Free-jet investigation of mechanically suppressed, high radius ratio coannular plug model nozzles [PDF]
The experimental and analytical acoustic results of a scale-model investigation or unsuppressed and mechanically suppressed high-radius ratio coannular plug nozzles with inverted velocity and temperature profiles are summarized.
Brausch, J. F. +3 more
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Evaluation of the Thermal Diffusivity of Carbon/Phenolic Composites (CPCs) through Oxy-Acetylene Torch (OAT) Test-Part 1: Experimental Characterization and Preliminary Validation. [PDF]
Polymers (Basel)Natali M, Torre L, Rallini M.
europepmc +1 more source
Variable stream control engine concept for advanced supersonic aircraft: Features and benefits [PDF]
The Variable Stream Control Engine is studied for advanced supersonic cruise aircraft. Significant environmental and performance improvements relative to first generation supersonic turbojet engines are cited.
Howlett, R. A.
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A preliminary design study of supersonic through-flow fan inlets [PDF]
From Mach 3.20 cruise propulsion systems, preliminary design studies for two supersonic through-flow fan primary inlets and a single core inlet were undertaken.
Barnhart, Paul J.
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From Classics to Nano-Excipients and Biopolymers: Pulmonary Drug Delivery Formulations. [PDF]
PharmaceuticsNikou M +3 more
europepmc +1 more source
Uncertainty and Traceability for the CEESI Iowa Natural Gas Facility. [PDF]
J Res Natl Inst Stand Technol, 2004 Johnson A, Kegel T.
europepmc +1 more source
Design and evaluation of an integrated Quiet, Clean General Aviation Turbofan (QCGAT) engine and aircraft propulsion system [PDF]
The design was based on the LTS-101 engine family for the core engine. A high bypass fan design (BPR=9.4) was incorporated to provide reduced fuel consumption for the design mission. All acoustic and pollutant emissions goals were achieved.
Fogel, P., German, J., Wilson, C.
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Self-Emulsifying Drug Delivery Systems (SEDDS): Transition from Liquid to Solid-A Comprehensive Review of Formulation, Characterization, Applications, and Future Trends. [PDF]
PharmaceuticsUttreja P +9 more
europepmc +1 more source