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Supplementary Wind Tunnel Investigation Of The Stability Of The Jettisonable Nose Section Of The X 2 Airplane
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Book Synopsis Supplementary Wind-tunnel Investigation of the Stability of the Jettisonable Nose Section of the X-2 Airplane by : Roscoe H. Goodwin
Download or read book Supplementary Wind-tunnel Investigation of the Stability of the Jettisonable Nose Section of the X-2 Airplane written by Roscoe H. Goodwin and published by . This book was released on 1949 with total page 21 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation of the Stability of the Jettisonable Nose Section of the XS-2 Airplane by : Stanley H. Scher
Download or read book Wind-tunnel Investigation of the Stability of the Jettisonable Nose Section of the XS-2 Airplane written by Stanley H. Scher and published by . This book was released on 1948 with total page 27 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-Tunnel Investigation of the Stability of Jettisoned Nose Sections of the D-558 Airplane - Phases 1 and 2 by :
Download or read book Wind-Tunnel Investigation of the Stability of Jettisoned Nose Sections of the D-558 Airplane - Phases 1 and 2 written by and published by . This book was released on 1948 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation of the stability of models of the jettisonable sections of the D-558 airplanes was conducted in the Langley 20-foot-spinning tunnel. It was found that both model nose sections tumbled end over end about an approximately horizontal axis. The installation of suitable fins, together with sufficient forward location of the center of gravity, prevented the tumbling and caused the models to descend in a stable nosedown attitude.
Book Synopsis Index of NACA Technical Publications by : United States. National Advisory Committee for Aeronautics
Download or read book Index of NACA Technical Publications written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1959 with total page 388 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation of the Stability of Jettisoned Nose Sections of the D-558 Airplane - Phases I and II by : Stanley H. Scher
Download or read book Wind-tunnel Investigation of the Stability of Jettisoned Nose Sections of the D-558 Airplane - Phases I and II written by Stanley H. Scher and published by . This book was released on 1948 with total page 33 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation of the Static Stability of a 1/56-scale Model of the X-1E Airplane at Mach Numbers of 2.37, 2.98, and 4.01 by : Fred M. Smith
Download or read book Wind-tunnel Investigation of the Static Stability of a 1/56-scale Model of the X-1E Airplane at Mach Numbers of 2.37, 2.98, and 4.01 written by Fred M. Smith and published by . This book was released on 1959 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Selected Listing of NASA Scientific and Technical Reports for ... by :
Download or read book A Selected Listing of NASA Scientific and Technical Reports for ... written by and published by . This book was released on 1957 with total page 388 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis WIND-TUNNEL INVESTIGATION OF DEVICES TO IMPROVE STATIC DIRECTIONAL STABILITY OF AN UNSWEPT-WING AIRPLANE MODEL AT MACH NUMBERS FROM 0.8 TO 2.2 by : Ralph W. Holtzclaw
Download or read book WIND-TUNNEL INVESTIGATION OF DEVICES TO IMPROVE STATIC DIRECTIONAL STABILITY OF AN UNSWEPT-WING AIRPLANE MODEL AT MACH NUMBERS FROM 0.8 TO 2.2 written by Ralph W. Holtzclaw and published by . This book was released on 1958 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis WIND-TUNNEL INVESTIGATION OF THE STATIC STABILITY OF A 1 56-SCALE MODEL OF THE X-1E AIRPLANE AT MACH NUMBERS OF 2.37, 2.98, AND 4.01 by :
Download or read book WIND-TUNNEL INVESTIGATION OF THE STATIC STABILITY OF A 1 56-SCALE MODEL OF THE X-1E AIRPLANE AT MACH NUMBERS OF 2.37, 2.98, AND 4.01 written by and published by . This book was released on 1959 with total page 128 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Subsonic Wind-tunnel Investigation of Errors Indicated by Total-pressure Tubes in the Flow Field of a Body Simulating the Nose of the X-15 Research Airplane by : William J. Alford
Download or read book Subsonic Wind-tunnel Investigation of Errors Indicated by Total-pressure Tubes in the Flow Field of a Body Simulating the Nose of the X-15 Research Airplane written by William J. Alford and published by . This book was released on 1962 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation at a Mach Number of 2.91 of Stability and Control Characteristics of Three Lifting Reentry Configurations at Angles of Attack Up to 90° by : John E. Grimaud
Download or read book Wind-tunnel Investigation at a Mach Number of 2.91 of Stability and Control Characteristics of Three Lifting Reentry Configurations at Angles of Attack Up to 90° written by John E. Grimaud and published by . This book was released on 1961 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation at Low Speed to Determine Aerodynamic Properties of a Jettisonable Nose Section with Circular Cross Section by : Roscoe H. Goodwin
Download or read book Wind-tunnel Investigation at Low Speed to Determine Aerodynamic Properties of a Jettisonable Nose Section with Circular Cross Section written by Roscoe H. Goodwin and published by . This book was released on 1950 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: The aerodynamic properties of a model of a jettisonable nose section with a circular cross section were determined at low speed from an investigation in the Langley 20-foot free-spinning tunnel.
Book Synopsis Wind Tunnel Investigation of an All Flush Orifice Air Data System for a Large Subsonic Aircraft by : Terry J. Larson
Download or read book Wind Tunnel Investigation of an All Flush Orifice Air Data System for a Large Subsonic Aircraft written by Terry J. Larson and published by . This book was released on 1980 with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind Tunnel Investigation of the Longitudinal Dynamic Stability of a Model Airplane by : Percy Hugh Francis Miller
Download or read book Wind Tunnel Investigation of the Longitudinal Dynamic Stability of a Model Airplane written by Percy Hugh Francis Miller and published by . This book was released on 1951 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-Tunnel Static and Free-Flight Investigation of High-Angle-Of-Attack Stability and Control Characteristics of a Model of the Ea-6b Airplane by : National Aeronautics and Space Adm Nasa
Download or read book Wind-Tunnel Static and Free-Flight Investigation of High-Angle-Of-Attack Stability and Control Characteristics of a Model of the Ea-6b Airplane written by National Aeronautics and Space Adm Nasa and published by . This book was released on 2018-11 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was conducted in the Langley 30- by 60-Foot Tunnel and the Langley 12-Foot Low-Speed Tunnel to identify factors contributing to a directional divergence at high angles of attack for the EA-6B airplane. The study consisted of static wind-tunnel tests, smoke and tuft flow-visualization tests, and free-flight tests of a 1/8.5-scale model of the airplane. The results of the investigation indicate that the directional divergence of the airplane is brought about by a loss of directional stability and effective dihedral at high angles of attack. Several modifications were tested that significantly alleviate the stability problem. The results of the free-flight study show that the modified configuration exhibits good dynamic stability characteristics and could be flown at angles of attack significantly higher than those of the unmodified configuration. Jordan, Frank L., Jr. and Hahne, David E. Langley Research Center...
Book Synopsis Wind-tunnel Investigation of the Effects of Various Dorsal-fin and Vertical-tail Configurations on the Directional Stability of a Streamlined Body at Transonic Speeds, Transonic-bump Method by : Harold S. Johnson
Download or read book Wind-tunnel Investigation of the Effects of Various Dorsal-fin and Vertical-tail Configurations on the Directional Stability of a Streamlined Body at Transonic Speeds, Transonic-bump Method written by Harold S. Johnson and published by . This book was released on 1953 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation of a Deflected-slipstream Cruise-fan V/STOL Aircraft Wing by : William A. Newsom
Download or read book Wind-tunnel Investigation of a Deflected-slipstream Cruise-fan V/STOL Aircraft Wing written by William A. Newsom and published by . This book was released on 1967 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
