Overview of Supersonic Laminar Flow Control Research on the F-16XL Ships 1 and 2

Overview of Supersonic Laminar Flow Control Research on the F-16XL Ships 1 and 2 PDF Author:
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Category :
Languages : en
Pages : 24

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Overview of Supersonic Laminar Flow Control Research on the F-16XL Ships 1 and 2

Overview of Supersonic Laminar Flow Control Research on the F-16XL Ships 1 and 2 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 24

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Boundary-layer Transition Results from the F-16XL-2 Supersonic Laminar Flow Control Experiment

Boundary-layer Transition Results from the F-16XL-2 Supersonic Laminar Flow Control Experiment PDF Author: Laurie A. Marshall
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ISBN:
Category : Boundary layer
Languages : en
Pages : 58

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A variable-porosity suction glove has been flown on the F-16XL-2 aircraft to demonstrate the feasibility of this technology for the proposed High-Speed Civil Transport (HSCT). Boundary-layer transition data have been obtained on the titanium glove primarily at Mach 2.0 and altitudes of 53,000-55,000 ft. The objectives of this supersonic laminar flow control flight experiment have been to achieve 50- to 60-percent-chord laminar flow on a highly swept wing at supersonic speeds and to provide data to validate codes and suction design. The most successful laminar flow results have not been obtained at the glove design point (Mach 1.9 at an altitude of 50,000 ft). At Mach 2.0 and an altitude of 53,000 ft, which corresponds to a Reynolds number of 22.7 multiplied by 10[factor 6], optimum suction levels have allowed long runs of a minimum of 46-percent-chord laminar flow to be achieved. This paper discusses research variables that directly impact the ability to obtain laminar flow and techniques to correct for these variables.

F-16XL-2 Supersonic Laminar Flow Control Flight Test Experiment

F-16XL-2 Supersonic Laminar Flow Control Flight Test Experiment PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 268

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 716

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Overview of Laminar Flow Control

Overview of Laminar Flow Control PDF Author: Ronald D. Joslin
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ISBN:
Category : Laminar flow
Languages : en
Pages : 146

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Flow and Noise Control: Review and Assessment of Future Directions

Flow and Noise Control: Review and Assessment of Future Directions PDF Author: Russell H. Thomas
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ISBN:
Category : Aerodynamical noise
Languages : en
Pages : 98

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NASA's Contributions to Aeronautics: Flight environment, operations, flight testing, and research

NASA's Contributions to Aeronautics: Flight environment, operations, flight testing, and research PDF Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 1064

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Two-volume collection of case studies on aspects of NACA-NASA research by noted engineers, airmen, historians, museum curators, journalists, and independent scholars. Explores various aspects of how NACA-NASA research took aeronautics from the subsonic to the hypersonic era.-publisher description.

NASA's Contributions to Aeronautics, Volume 2, Flight Environment ..., NASA/SP-2010-570-Vol 2, 2010, *

NASA's Contributions to Aeronautics, Volume 2, Flight Environment ..., NASA/SP-2010-570-Vol 2, 2010, * PDF Author:
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ISBN:
Category :
Languages : en
Pages : 1070

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Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author: United States. Superintendent of Documents
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ISBN:
Category : Government publications
Languages : en
Pages : 1072

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February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index

Monthly Catalogue, United States Public Documents

Monthly Catalogue, United States Public Documents PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 956

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