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Flight Wing Surface Pressure And Boundary Layer Data Report From The F 111 Smooth Variable Camber Supercritical Mission Adaptive Wing by Sheryll Goecke Powers

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1NASA Technical Reports Server (NTRS) 19970023528: Flight Wing Surface Pressure And Boundary-Layer Data Report From The F-111 Smooth Variable-Camber Supercritical Mission Adaptive Wing

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Flight tests were conducted using the advanced fighter technology integration F-111 (AFTI/F-111) aircraft modified with a variable-sweep supercritical mission adaptive wing (MAW). The MAW leading- and trailing-edge variable-camber surfaces were deflected in flight to provide a near-ideal wing camber shape for the flight condition. The MAW features smooth, flexible upper surfaces and fully enclosed lower surfaces, which distinguishes it from conventional flaps that have discontinuous surfaces and exposed or semi-exposed mechanisms. Upper and lower surface wing pressure distributions were measured along four streamwise rows on the right wing for cruise, maneuvering, and landing configurations. Boundary-layer measurements were obtained near the trailing edge for one of the rows. Cruise and maneuvering wing leading-edge sweeps were 26 deg for Mach numbers less than 1 and 45 deg or 58 deg for Mach numbers greater than 1. The landing wing sweep was 9 deg or 16 deg. Mach numbers ranged from 0.27 to 1.41, angles of attack from 2 deg to 13 deg, and Reynolds number per unit foot from 1.4 x 10(exp 6) to 6.5 x 10(exp 6). Leading-edge cambers ranged from O deg to 20 deg down, and trailing-edge cambers ranged from 1 deg up to 19 deg down. Wing deflection data for a Mach number of 0.85 are shown for three cambers. Wing pressure and boundary-layer data are given. Selected data comparisons are shown. Measured wing coordinates are given for three streamwise semispan locations for cruise camber and one spanwise location for maneuver camber.

“NASA Technical Reports Server (NTRS) 19970023528: Flight Wing Surface Pressure And Boundary-Layer Data Report From The F-111 Smooth Variable-Camber Supercritical Mission Adaptive Wing” Metadata:

  • Title: ➤  NASA Technical Reports Server (NTRS) 19970023528: Flight Wing Surface Pressure And Boundary-Layer Data Report From The F-111 Smooth Variable-Camber Supercritical Mission Adaptive Wing
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  • Language: English

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1Practical Guide to Self-Hypnosis

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Summary from <em>A Practical Guide to Self-Hypnosis</em>: This book is written in terms that are comprehensible to the layman. The step-by-step instructions should afford the reader a means of acquiring self-hypnosis. The necessary material is here. The reader need only follow the instructions as they are given. It is the author's hope that you will, through the selective use of self-hypnosis, arrive at a more rewarding, well-adjusted, and fuller life.

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  • Title: ➤  Practical Guide to Self-Hypnosis
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  • Format: Audio
  • Number of Sections: 13
  • Total Time: 3:48:02

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  • Number of Sections: 13 sections

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2Stories the Iroquois Tell Their Children

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Stories the Iroquois Tell Their Children by Mabel Powers is a beautiful collection of traditional Iroquois tales that not only entertain but also teach fundamental cultural values and life lessons. These stories, passed down through generations by elders around the fire, serve to educate children on themes such as bravery, kindness, respect for nature, and the importance of community. The book’s tales feature a range of characters including the Little People, animals, and children. Each story is rich with symbolic meaning. Powers also touches on the role of nature in these stories, reflecting the Iroquois' deep reverence for the natural world and its creatures, while exploring concepts like gratitude, generosity, and cooperation. By weaving together these ancient tales with lessons about life, the book offers not only a glimpse into Iroquois culture but also timeless wisdom that transcends generations. - Summary by Anthony Karl Futterer

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  • Title: ➤  Stories the Iroquois Tell Their Children
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  • Language: English
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  • Format: Audio
  • Number of Sections: 39
  • Total Time: 03:02:25

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  • Number of Sections: 39 sections

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