Design of a High Angle of Attack Robotic Sting Mount for Tests in a Low Speed Wind Tunnel

Design of a High Angle of Attack Robotic Sting Mount for Tests in a Low Speed Wind Tunnel PDF Author: Tommy Jack Kubler
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 286

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Book Description
A sting mounting system designed for high angle of attack (AOA) testing has been developed for the 7x10 foot low-speed wind tunnel (LSWT). The mechanism was able to position the model from -15 deg to +90 deg of pitch with accuracy to within 0.2 deg, while keeping the model near the center of the test section. Compatible with the current turntable apparatus, the high angle of attack robotic sting (HARS) retained the turntable's full range of yaw movement of + or - 90 deg. All model positioning was done without shutting the tunnel down to manually alter the sting or mounting apparatus. Pitch adjustment progressed at about 4 deg per second, with final position tuning taking nearly 15 seconds. The mechanism consisted of two square steel telescoping tube struts that were joined at the ends in the test section by a cross link that held the existing LSWT small Langley sting. Wind tunnel blockage and flow irregularities near the model were minimized by mounting drive hardware under the tunnel floor. An IBM/AT compatible microcomputer equipped with an analog-to-digital conversion board provided position control, drive motor signaling, and input signal filtering. Theses. (jhd).

Design of a High Angle of Attack Robotic Sting Mount for Tests in a Low Speed Wind Tunnel

Design of a High Angle of Attack Robotic Sting Mount for Tests in a Low Speed Wind Tunnel PDF Author: Tommy Jack Kubler
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 286

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Book Description
A sting mounting system designed for high angle of attack (AOA) testing has been developed for the 7x10 foot low-speed wind tunnel (LSWT). The mechanism was able to position the model from -15 deg to +90 deg of pitch with accuracy to within 0.2 deg, while keeping the model near the center of the test section. Compatible with the current turntable apparatus, the high angle of attack robotic sting (HARS) retained the turntable's full range of yaw movement of + or - 90 deg. All model positioning was done without shutting the tunnel down to manually alter the sting or mounting apparatus. Pitch adjustment progressed at about 4 deg per second, with final position tuning taking nearly 15 seconds. The mechanism consisted of two square steel telescoping tube struts that were joined at the ends in the test section by a cross link that held the existing LSWT small Langley sting. Wind tunnel blockage and flow irregularities near the model were minimized by mounting drive hardware under the tunnel floor. An IBM/AT compatible microcomputer equipped with an analog-to-digital conversion board provided position control, drive motor signaling, and input signal filtering. Theses. (jhd).

Masters Theses in the Pure and Applied Sciences

Masters Theses in the Pure and Applied Sciences PDF Author: Wade H. Shafer
Publisher: Springer Science & Business Media
ISBN: 1461534747
Category : Science
Languages : en
Pages : 421

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Book Description
Masters Theses in the Pure and Applied Sciences was first conceived, published, and disseminated by the Center for Information and Numerical Data Analysis and Synthesis (CINDAS) * at Purdue University in 1957, starting its coverage of theses with the academic year 1955. Beginning with Volume 13, the printing and dissemination phases of the activity were transferred to University Microfilms/Xerox of Ann Arbor, Michigan, with the thought that such an arrangement would be more beneficial to the academic and general scientific and technical community. After five years of this joint undertaking we had concluded that it was in the interest of all con cerned if the printing and distribution of the volumes were handled by an interna tional publishing house to assure improved service and broader dissemination. Hence, starting with Volume 18, Masters Theses in the Pure and Applied Sciences has been disseminated on a worldwide basis by Plenum Publishing Cor poration of New York, and in the same year the coverage was broadened to include Canadian universities. All back issues can also be ordered from Plenum. We have reported in Volume 34 (thesis year 1989) a total of 13,377 theses titles from 26 Canadian and 184 United States universities. We are sure that this broader base for these titles reported will greatly enhance the value of this important annual reference work. While Volume 34 reports theses submitted in 1989, on occasion, certain univer sities do report theses submitted in previous years but not reported at the time.

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 268

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NASA SP.

NASA SP. PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 468

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Aeronautical Engineering

Aeronautical Engineering PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 568

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Book Description
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).

Government Reports Announcements & Index

Government Reports Announcements & Index PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1178

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Government Reports Annual Index

Government Reports Annual Index PDF Author:
Publisher:
ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 1102

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Research Centers Directory

Research Centers Directory PDF Author:
Publisher:
ISBN:
Category : Canada
Languages : en
Pages : 1254

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Book Description
Research institutes, foundations, centers, bureaus, laboratories, experiment stations, and other similar nonprofit facilities, organizations, and activities in the United States and Canada. Entry gives identifying and descriptive information of staff and work. Institutional, research centers, and subject indexes. 5th ed., 5491 entries; 6th ed., 6268 entries.

Dissertation Abstracts International

Dissertation Abstracts International PDF Author:
Publisher:
ISBN:
Category : Dissertations, Academic
Languages : en
Pages : 716

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International Aerospace Abstracts

International Aerospace Abstracts PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 530

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