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Low Speed Wind Tunnel Investigation Of The Stability And Control Characteristics Of A Series Of Flying Wings With Sweep Angles Of 60 Deg
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Book Synopsis Low-speed Wind Tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 60 Degrees by : Thomas M. Moul
Download or read book Low-speed Wind Tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 60 Degrees written by Thomas M. Moul and published by . This book was released on 1995 with total page 156 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Adm Nasa Publisher :Independently Published ISBN 13 :9781731367068 Total Pages :160 pages Book Rating :4.3/5 (67 download)
Book Synopsis Low-Speed Wind Tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 60 Deg by : National Aeronautics and Space Adm Nasa
Download or read book Low-Speed Wind Tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 60 Deg written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2018-11-18 with total page 160 pages. Available in PDF, EPUB and Kindle. Book excerpt: A wind tunnel investigation was conducted in the Langley 12-Foot Low-Speed Wind Tunnel to study the low-speed stability and control characteristics of a series of four flying wings over an extended range of angle of attack (-8 deg to 48 deg). Because of the current emphasis on reducing the radar cross section of new military aircraft, the planform of each wing was composed of lines swept at a relatively high angle of 60 deg, and all the trailing-edge lines were aligned with one of the two leading edges. Three arrow planforms with different aspect ratios and one diamond planform were tested. The models incorporated leading-edge flaps for improved pitching-moment characteristics and lateral stability and had three sets of trailing-edge flaps that were deflected differentially for roll control, symmetrically for pitch control, and in a split fashion for yaw control. Top bodies of three widths and twin vertical tails of various sizes and locations were also tested on each model. A large aerodynamic database was compiled that could be used to evaluate some of the trade-offs involved in the design of a configuration with a reduced radar cross section and good flight dynamic characteristics. Moul, Thomas M. and Fears, Scott P. and Ross, Holly M. and Foster, John V. Langley Research Center AIRCRAFT DESIGN; DIRECTIONAL STABILITY; FLIGHT CHARACTERISTICS; LATERAL STABILITY; LEADING EDGE FLAPS; LOW SPEED STABILITY; RADAR CROSS SECTIONS; SWEPTBACK WINGS; TAIL ASSEMBLIES; TAILLESS AIRCRAFT; TRAILING EDGE FLAPS; WIND TUNNEL TESTS; ANGLE OF ATTACK; ASPECT RATIO; LEADING EDGES; PITCHING MOMENTS; ROLLING MOMENTS; TRADEOFFS; TRAILING EDGES; YAW...
Book Synopsis Low-speed Wind Tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 60 Deg by :
Download or read book Low-speed Wind Tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 60 Deg written by and published by . This book was released on 1995 with total page 174 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781723196645 Total Pages :158 pages Book Rating :4.1/5 (966 download)
Book Synopsis Low-Speed Wind Tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 60 Deg by : National Aeronautics and Space Administration (NASA)
Download or read book Low-Speed Wind Tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 60 Deg written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-18 with total page 158 pages. Available in PDF, EPUB and Kindle. Book excerpt: A wind tunnel investigation was conducted in the Langley 12-Foot Low-Speed Wind Tunnel to study the low-speed stability and control characteristics of a series of four flying wings over an extended range of angle of attack (-8 deg to 48 deg). Because of the current emphasis on reducing the radar cross section of new military aircraft, the planform of each wing was composed of lines swept at a relatively high angle of 60 deg, and all the trailing-edge lines were aligned with one of the two leading edges. Three arrow planforms with different aspect ratios and one diamond planform were tested. The models incorporated leading-edge flaps for improved pitching-moment characteristics and lateral stability and had three sets of trailing-edge flaps that were deflected differentially for roll control, symmetrically for pitch control, and in a split fashion for yaw control. Top bodies of three widths and twin vertical tails of various sizes and locations were also tested on each model. A large aerodynamic database was compiled that could be used to evaluate some of the trade-offs involved in the design of a configuration with a reduced radar cross section and good flight dynamic characteristics. Moul, Thomas M. and Fears, Scott P. and Ross, Holly M. and Foster, John V. Langley Research Center AIRCRAFT DESIGN; DIRECTIONAL STABILITY; FLIGHT CHARACTERISTICS; LATERAL STABILITY; LEADING EDGE FLAPS; LOW SPEED STABILITY; RADAR CROSS SECTIONS; SWEPTBACK WINGS; TAIL ASSEMBLIES; TAILLESS AIRCRAFT; TRAILING EDGE FLAPS; WIND TUNNEL TESTS; ANGLE OF ATTACK; ASPECT RATIO; LEADING EDGES; PITCHING MOMENTS; ROLLING MOMENTS; TRADEOFFS; TRAILING EDGES; YAW...
Book Synopsis Low-speed Wind-tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 60 ̊ by :
Download or read book Low-speed Wind-tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 60 ̊ written by and published by . This book was released on 1995 with total page 155 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low-speed Wind-tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 70 Deg by :
Download or read book Low-speed Wind-tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 70 Deg written by and published by . This book was released on 1995 with total page 148 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low-speed Wind-tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 50 Deg by :
Download or read book Low-speed Wind-tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 50 Deg written by and published by . This book was released on 1995 with total page 152 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low-speed Wind Tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 50 Degrees by : Scott P. Fears
Download or read book Low-speed Wind Tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 50 Degrees written by Scott P. Fears and published by . This book was released on 1995 with total page 146 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781723196812 Total Pages :144 pages Book Rating :4.1/5 (968 download)
Book Synopsis Low-Speed Wind-Tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 70 Deg by : National Aeronautics and Space Administration (NASA)
Download or read book Low-Speed Wind-Tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 70 Deg written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-18 with total page 144 pages. Available in PDF, EPUB and Kindle. Book excerpt: A wind-tunnel investigation was conducted in the Langley 12-Foot Low-Speed Tunnel to study the low-speed stability and control characteristics of a series of four flying wings over an extended range of angle of attack (-8 deg to 48 deg). Because of the current emphasis on reducing the radar cross section (RCS) of new military aircraft, the planform of each wing was composed of lines swept at a relatively high angle of 70 deg, and all the trailing edges and control surface hinge lines were aligned with one of the two leading edges. Three arrow planforms with different aspect ratios and one diamond planform were tested. The models incorporated leading-edge flaps for improved longitudinal characteristics and lateral stability and had three sets of trailing-edge flaps that were deflected differentially for roll control, symmetrically for pitch control, and in a split fashion for yaw control. Three top body widths and two sizes of twin vertical tails were also tested on each model. A large aerodynamic database was compiled that could be used to evaluate some of the trade-offs involved in the design of a configuration with a reduced RCS and good flight dynamic characteristics. Ross, Holly M. and Fears, Scott P. and Moul, Thomas M. Langley Research Center ANGLE OF ATTACK; ARROW WINGS; DYNAMIC CHARACTERISTICS; LOW ASPECT RATIO WINGS; LOW SPEED; RADAR CROSS SECTIONS; SIDESLIP; TAILLESS AIRCRAFT; WIND TUNNEL TESTS; ASPECT RATIO; LATERAL CONTROL; LATERAL STABILITY; LEADING EDGE FLAPS; LONGITUDINAL STABILITY; TAIL ASSEMBLIES; TRAILING EDGE FLAPS...
Book Synopsis Low-speed Wind-tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 70 Degrees by : Holly M. Ross
Download or read book Low-speed Wind-tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 70 Degrees written by Holly M. Ross and published by . This book was released on 1995 with total page 140 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low-speed Wind-tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 50 ̊ by : Scott P. Fears
Download or read book Low-speed Wind-tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 50 ̊ written by Scott P. Fears and published by . This book was released on 1995 with total page 145 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low-speed Wind-tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 70 ̊ by : Holly M. Ross
Download or read book Low-speed Wind-tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 70 ̊ written by Holly M. Ross and published by . This book was released on 1995 with total page 140 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low-speed Wind-tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 70 by : Holly M. Ross
Download or read book Low-speed Wind-tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 70 written by Holly M. Ross and published by . This book was released on 1995 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low-speed Wind-tunnnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 60 Degrees by : Thomas M. Moul
Download or read book Low-speed Wind-tunnnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 60 Degrees written by Thomas M. Moul and published by . This book was released on 1995 with total page 155 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Preliminary Wind-tunnel Investigation at Low Speed of Stability and Control Characteristics of Swept-back Wings by : William Letko
Download or read book Preliminary Wind-tunnel Investigation at Low Speed of Stability and Control Characteristics of Swept-back Wings written by William Letko and published by . This book was released on 1946 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tests were conducted on untapered constant-span wings of 0, 30, 45, and 60 degree sweepback. The purpose of these tests was to investigate the effect of sweepback on stability and control characteristics.
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 704 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :United States. National Aeronautics and Space Administration. Scientific and Technical Information Division Publisher : ISBN 13 : Total Pages :2088 pages Book Rating :4.E/5 ( download)
Book Synopsis A Selected Listing of NASA Scientific and Technical Reports for ... by : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Download or read book A Selected Listing of NASA Scientific and Technical Reports for ... written by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division and published by . This book was released on 1966 with total page 2088 pages. Available in PDF, EPUB and Kindle. Book excerpt:
