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Reynolds Number Effects On Leading Edge Radius Variations Of A Supersonic Transport At Transonic Conditions
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Book Synopsis Reynolds Number Effects on Leading Edge Radius Variations of a Supersonic Transport at Transonic Conditions by : S. M. B. Rivers
Download or read book Reynolds Number Effects on Leading Edge Radius Variations of a Supersonic Transport at Transonic Conditions written by S. M. B. Rivers and published by . This book was released on 2001 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781721089703 Total Pages :110 pages Book Rating :4.0/5 (897 download)
Book Synopsis A Reynolds Number Study of Wing Leading-Edge Effects on a Supersonic Transport Model at Mach 0. 3 by : National Aeronautics and Space Administration (NASA)
Download or read book A Reynolds Number Study of Wing Leading-Edge Effects on a Supersonic Transport Model at Mach 0. 3 written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-06-13 with total page 110 pages. Available in PDF, EPUB and Kindle. Book excerpt: A representative supersonic transport design was tested in the National Transonic Facility (NTF) in its original configuration with small-radius leading-edge flaps and also with modified large-radius inboard leading-edge flaps. Aerodynamic data were obtained over a range of Reynolds numbers at a Mach number of 0.3 and angles of attack up to 16 deg. Increasing the radius of the inboard leading-edge flap delayed nose-up pitching moment to a higher lift coefficient. Deflecting the large-radius leading-edge flap produced an overall decrease in lift coefficient and delayed nose-up pitching moment to even higher angles of attack as compared with the undeflected large- radius leading-edge flap. At angles of attack corresponding to the maximum untrimmed lift-to-drag ratio, lift and drag coefficients decreased while lift-to-drag ratio increased with increasing Reynolds number. At an angle of attack of 13.5 deg., the pitching-moment coefficient was nearly constant with increasing Reynolds number for both the small-radius leading-edge flap and the deflected large-radius leading-edge flap. However, the pitching moment coefficient increased with increasing Reynolds number for the undeflected large-radius leading-edge flap above a chord Reynolds number of about 35 x 10 (exp 6). Williams, M. Susan and Owens, Lewis R., Jr. and Chu, Julio Langley Research Center RTOP 537-03-22-06
Book Synopsis A Reynolds Number Study of Wing Leading-Edge Effects on a Supersonic Transport Model at Mach 0.3 by : M. Susan Williams
Download or read book A Reynolds Number Study of Wing Leading-Edge Effects on a Supersonic Transport Model at Mach 0.3 written by M. Susan Williams and published by . This book was released on 1999 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt: A representative supersonic transport design was tested in the National Transonic Facility (NTF) in its original configuration with small-radius leading-edge flaps and also with modified large-radius inboard leading-edge flaps. Aerodynamic data were obtained over a range of Reynolds numbers at a Mach number of 0.3 and angles of attack up to 16 deg. Increasing the radius of the inboard leading-edge flap delayed nose-up pitching moment to a higher lift coefficient. Deflecting the large-radius leading-edge flap produced an overall decrease in lift coefficient and delayed nose-up pitching moment to even higher angles of attack as compared with the undeflected large- radius leading-edge flap. At angles of attack corresponding to the maximum untrimmed lift-to-drag ratio, lift and drag coefficients decreased while lift-to-drag ratio increased with increasing Reynolds number. At an angle of attack of 13.5 deg., the pitching-moment coefficient was nearly constant with increasing Reynolds number for both the small-radius leading-edge flap and the deflected large-radius leading-edge flap. However, the pitching moment coefficient increased with increasing Reynolds number for the undeflected large-radius leading-edge flap above a chord Reynolds number of about 35 x 10 (exp 6).
Book Synopsis Reynolds Number Effects on a Supersonic Transport at Transonic Conditions by : R. A. Wahls
Download or read book Reynolds Number Effects on a Supersonic Transport at Transonic Conditions written by R. A. Wahls and published by . This book was released on 2001 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Leading-edge Contour and Vertical-tail Configuration on the Low-speed Stability Characteristics of a Supersonic Transport Model Having a Highly-swept Arrow Wing by :
Download or read book Effect of Leading-edge Contour and Vertical-tail Configuration on the Low-speed Stability Characteristics of a Supersonic Transport Model Having a Highly-swept Arrow Wing written by and published by . This book was released on 1978 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Aerodynamic Characteristics of a Tailless Fixed-wing Supersonic Transport Model by : Edward J. Ray
Download or read book Transonic Aerodynamic Characteristics of a Tailless Fixed-wing Supersonic Transport Model written by Edward J. Ray and published by . This book was released on 1966 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis NASA's Contributions to Aeronautics: Flight environment, operations, flight testing, and research by :
Download or read book NASA's Contributions to Aeronautics: Flight environment, operations, flight testing, and research written by and published by . This book was released on 2010 with total page 1064 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis NASA's Contributions to Aeronautics, Volume 2, Flight Environment ..., NASA/SP-2010-570-Vol 2, 2010, * by :
Download or read book NASA's Contributions to Aeronautics, Volume 2, Flight Environment ..., NASA/SP-2010-570-Vol 2, 2010, * written by and published by . This book was released on 2011 with total page 1070 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Reynolds Number Effects on a Supersonic Transport at Subsonic High-lift Conditions by : L. R. Owens
Download or read book Reynolds Number Effects on a Supersonic Transport at Subsonic High-lift Conditions written by L. R. Owens and published by . This book was released on 2001 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis NASA Langley Scientific and Technical Information Output-2001 by :
Download or read book NASA Langley Scientific and Technical Information Output-2001 written by and published by . This book was released on 2002 with total page 166 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low-speed Effects of High-lift Devices on the Aerodynamic Characteristics of a Supersonic Transport Model with Outboard Tails by : William C. Sleeman
Download or read book Low-speed Effects of High-lift Devices on the Aerodynamic Characteristics of a Supersonic Transport Model with Outboard Tails written by William C. Sleeman and published by . This book was released on 1963 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Comparison of Transition Reynolds Numbers from 12-in. and 40-in. Supersonic Tunnels by : C. J. Schueler
Download or read book A Comparison of Transition Reynolds Numbers from 12-in. and 40-in. Supersonic Tunnels written by C. J. Schueler and published by . This book was released on 1963 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: Transition Reynolds number measurements on a hollow cylinder in the von Karman Gas Dynamics Facility's 12-inch and 40-inch supersonic tunnels show that the highest transition Reynolds numbers were obtained in the 40-inch tunnel, although the variations with unit Reynolds number were the same at Mach numbers 3 to 5. The influence of nose bluntness in the 40-inch tunnel corresponds closely with the results obtained in the 12-inch tunnel.
Download or read book NASA Reference Publication written by and published by . This book was released on 1977 with total page 1092 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 39th AIAA Aerospace Sciences Meeting and Exhibit by :
Download or read book 39th AIAA Aerospace Sciences Meeting and Exhibit written by and published by . This book was released on 2001 with total page 656 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Effects of Model Scale and Stream Reynolds Number on the Aerodynamic Characteristics of Two Rectangular Wings at Supersonic Speeds on the Langley 9-inch Supersonic Tunnel by : Donald E. Coletti
Download or read book Investigation of the Effects of Model Scale and Stream Reynolds Number on the Aerodynamic Characteristics of Two Rectangular Wings at Supersonic Speeds on the Langley 9-inch Supersonic Tunnel written by Donald E. Coletti and published by . This book was released on 1955 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Subsonic, Transonic, and Supersonic Aerodynamic Characteristics of a Modified Arrow-wing Transport Airplane Configuration by :
Download or read book Subsonic, Transonic, and Supersonic Aerodynamic Characteristics of a Modified Arrow-wing Transport Airplane Configuration written by and published by . This book was released on 1964 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :Richard Hallion Publisher :National Aeronautics and Space Administration Headquarters ISBN 13 : Total Pages :1064 pages Book Rating :4.3/5 (243 download)
Book Synopsis NASA's Contributions to Aeronautics by : Richard Hallion
Download or read book NASA's Contributions to Aeronautics written by Richard Hallion and published by National Aeronautics and Space Administration Headquarters. This book was released on 2010 with total page 1064 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
