62 research outputs found
Effect of Desmodium adscendens fraction 3 on contractions of respiratory smooth muscle
No full textPT: J; CR: ADDY ME, 1984, J ETHNOPHARMACOL, V11, P283 ADDY ME, 1986, J ETHNOPHARMACOL, V18, P13 ADDY ME, 1987, PHYTOTHER RES, V1, P180 ADDY ME, 1988, CAN J PHYSL PHARM, V66, P820 ADDY ME, 1989, INT J CRUDE DRUG RES, V27, P81 BURKA JF, 1983, J PHARMACOL EXP THER, V225, P427 CONSTANTINE JW, 1965, J PHARM PHARMACOL, V17, P384 DARIUS H, 1986, SCIENCE, V232, P58 LULICH KM, 1979, CLIN EXP PHARM PHYSL, V6, P625 OREHEK J, 1975, J PHARMACOL EXP THER, V194, P554 PIPER PJ, 1982, BRIT J PHARMACOL, V77, P267 SAAD MH, 1983, CAN J PHYSIOL PHARM, V61, P876 STILL WC, 1978, J ORG CHEM, V43, P2923 ZIJLSTRA FJ, 1984, AGENTS ACTIONS, V14, P88; NR: 14; TC: 5; J9: J ETHNOPHARMACOL; PG: 11; GA: DN792Source type: Electronic(1
Effect of Desmodium adscendens fraction F1 (DAF1) on tone and agonist-induced contractions of guinea pig airway smooth muscle
No full textPT: J; CR: ADDY ME, 1984, J ETHNOPHARMACOL, V11, P283 ADDY ME, 1986, J ETHNOPHARMACOL, V18, P13 ADDY ME, 1987, PHYTOTHER RES, V1, P1080 BURKA JF, 1985, PROSTAGLANDINS, V29, P529 CONSTANTINE JW, 1965, J PHARM PHARMACOL, V17, P384 LULICH KM, 1979, CLIN EXP PHARM PHYSL, V6, P625 OREHEK J, 1973, NATURE-NEW BIOL, V245, P84 SAAD MH, 1983, CAN J PHYSIOL PHARM, V61, P876 SAMUELSSON B, 1983, SCIENCE, V220, P568 SCHULMAN ES, 1982, J APPL PHYSIOL, V53, P589 STILL WC, 1978, J ORG CHEM, V43, P2923 WASSERMAN MA, 1983, ADV PROSTAGLANDIN TH, V12, P133; NR: 12; TC: 8; J9: PHYTOTHER RES; PG: 6; GA: AX428Source type: Electronic(1
Small Steps for Building More Inclusive Classrooms
No full textInclusive instruction is critical to build welcoming and equitable experiences for diverse learners. Addy demonstrates through an interactive session how instructors can take small steps toward creating inclusive environments for their students.
“Dr. Addy is a leading voice on inclusive teaching and faculty development,” said Laura Taylor, associate professor of theology at CSB and SJU, who is director of the Center for Learning and Teaching. “It is a big deal that she is coming to work with our faculty. I feel so fortunate that we are able to host her on campus as part of this series.”
Addy received her bachelor’s degree from Duke University, then earned a master’s in philosophy from Yale University and a Ph.D. in science education at North Carolina State University. She also taught at the undergraduate level for 10 years. At Lafayette, she is responsible for working with instructors to develop and administer programming. She is director of the Center for the Integration of Teaching, Learning and Scholarship. The Center focuses on inclusivity for instructors and integrating students as partners.
Addy’s work has been featured in academic journals and other publications, like Inside Higher Ed and University Business. She is co-author of What Inclusive Instructors Do: Principles and Practices for Excellence in College Teaching, printed in 2021 by Stylus Publishing
Operationalizing Occupation-Centered Education: Exploring the Subject-Centered Integrative Learning Model in Academic Education
No full textAbstract
Date Presented 4/1/2017
The purpose of this study was to explore the usefulness of the Subject-Centered Integrative Learning Model for academic educators developing occupation-centered practices. The model was found to guide the educators and has the potential to shape occupational therapy education.
Primary Author and Speaker: Addy Brown
Additional Authors and Speakers: Barbara Hooper, Devin Barth, Amanda Zorn</jats:p
History of St. Anthony's School
No full textBooklet - The front cover of the History of St. Anthony's School September 1959-May 1985 accompanied by a letter of thanks from Addy Contenti, Chairman of St. Anthony's School Board, Drumheller, AB, addressed to Mrs. Ella Zakariasen (2 pages
Jazz & Blues Festival: A Feast For Famished Fans
No full textLocations: EXPO Centre, Granville Island Band Shell, The Savoy (6 Powell St.), Landmark Jazz Bar (1400 Robson St.), Hot Jazz Club (2120 Main St.), Classical Joint (231 Carrall St.), Town Pump (66 Water St.). Obo Addy (drums); Aladar Pege (bass); "Kate Hammet-Vaughan (vox) Quintet;" "Paul Plimley (piano, vibes) Octet;" "Lunar Adventures.
Effect of Desmodium adscendens fractions on antigen- and arachidonic acid-induced contractions of guinea pig airways
No full textThree fractions (n-butanol, F2, and L5), isolated from an aqueous extract of Desmodium adscendens, a plant used in Ghana for the management of asthma, were evaluated for their pharmacological activity using ovalbumin and arachidonic acid-induced contractions of guinea pig airways. All three fractions inhibited the ovalbumin-induced contractions of indomethacin-pretreated tracheal spirals from sensitized animals dose dependently, but only L5 and n-butanol inhibited such contractions in the absence of indomethacin. The concentrations required to inhibit ovalbumin-induced contractions of lung parenchymal strips were threefold higher than with trachea. The contractile response over a 60-min period was divided into three phases. F2 and n-butanol inhibited all phases, whereas L5 inhibited only the late phase. n-Butanol and L5 inhibited arachidonic acid-induced contractions on indomethacin-pretreated tracheal spirals, a leukotriene-dependent reaction. There was no inhibition of arachidonic acid-induced contractions of lung parenchymal strips, which is largely a thromboxane-dependent reaction. The results suggest that D. adscendens contains several pharmacologically active substances that can inhibit allergic airway smooth muscle contraction at multiple sites, including the synthesis and (or) activity of the bronchoconstrictor leukotrienes.LR: 20061115; PUBM: Print; JID: 0372712; 0 (Arachidonic Acids); 0 (Butanols); 0 (Plant Extracts); 506-32-1 (Arachidonic Acid); 53-86-1 (Indomethacin); 71-36-3 (1-Butanol); 9006-59-1 (Ovalbumin); ppublishSource type: Electronic(1
Numerical calculations for flows past an unconventional airfoil
No full textA computer program has been developed for both two-dimensional compressible and incompressible turbulent flows around airfoils. Numerical solutions have been obtained by solving the steady-state Reynolds-averaged Navier-Stokes equations in primitive variable form. The standard k- turbulence model was employed and a compression turbulence model was also discussed. Based on a non-staggered arrangement on a body-fitted grid system, the discretized transport equations were solved either by a hybrid or a second-order upwind differencing scheme. A multiple pressure correction procedure with implicit density treatment has been used. The solutions were obtained through an under-relaxed iterative process.Various cases of flow past NACA 0012 and 4412 airfoils were examined first. The experimental data available included cases with freestream Mach numbers varying from 0 to 0.799, the chord Reynolds number up to 9 10\sp6, and the angle of attack ranging from 0\sp\circ to 13.87\sp\circ. The results were good when compared with experimental data. Many cases of incompressible and compressible flows past an unconventional airfoil were then computed. The freestream Mach number varied from 0 to 0.9 with the chord Reynolds number of 3.9 10\sp6. The general behavior of the unconventional airfoil is presented.Made available in DSpace on 2011-05-07T12:32:58Z (GMT). No. of bitstreams: 2
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Dose-response effects of one subfraction of Desmodium adscendens aqueous extract on antigen- and arachidonic acid-induced contractions of guinea pig airways
No full textSource type: Print(0
Numerical calculations for flows past an unconventional airfoil
No full textA computer program has been developed for both two-dimensional compressible and incompressible turbulent flows around airfoils. Numerical solutions have been obtained by solving the steady-state Reynolds-averaged Navier-Stokes equations in primitive variable form. The standard k- turbulence model was employed and a compression turbulence model was also discussed. Based on a non-staggered arrangement on a body-fitted grid system, the discretized transport equations were solved either by a hybrid or a second-order upwind differencing scheme. A multiple pressure correction procedure with implicit density treatment has been used. The solutions were obtained through an under-relaxed iterative process.Various cases of flow past NACA 0012 and 4412 airfoils were examined first. The experimental data available included cases with freestream Mach numbers varying from 0 to 0.799, the chord Reynolds number up to 9 10\sp6, and the angle of attack ranging from 0\sp\circ to 13.87\sp\circ. The results were good when compared with experimental data. Many cases of incompressible and compressible flows past an unconventional airfoil were then computed. The freestream Mach number varied from 0 to 0.9 with the chord Reynolds number of 3.9 10\sp6. The general behavior of the unconventional airfoil is presented.U of I OnlyETDs are only available to UIUC Users without author permissio
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