Wind-tunnel Investigation of Paraglider Models at Supersonic Speeds

Download Wind-tunnel Investigation of Paraglider Models at Supersonic Speeds PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 22 pages
Book Rating : 4.:/5 (31 download)

DOWNLOAD NOW!


Book Synopsis Wind-tunnel Investigation of Paraglider Models at Supersonic Speeds by : Robert T. Taylor

Download or read book Wind-tunnel Investigation of Paraglider Models at Supersonic Speeds written by Robert T. Taylor and published by . This book was released on 1961 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made in the Langley Unitary Plan wind tunnel to determine the behavior of paraglider models at moderate to high supersonic speeds. The models were deployed from a sting in the supersonic stream and steady-state aerodynamics performance data were obtained. Maximum values of the lift-drag ratio were about 1.4 at a Mach number of 2.65 and about 1.2 at a Mach number of 4.65. The angles of attack over which the models could be flown were limited by unsteady behavior of the canopy.

Wind-tunnel Investigation of Paraglider Models at Supersonic Speeds

Download Wind-tunnel Investigation of Paraglider Models at Supersonic Speeds PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (689 download)

DOWNLOAD NOW!


Book Synopsis Wind-tunnel Investigation of Paraglider Models at Supersonic Speeds by : Robert T. Taylor (Of the National Aeronautics and Space Administration)

Download or read book Wind-tunnel Investigation of Paraglider Models at Supersonic Speeds written by Robert T. Taylor (Of the National Aeronautics and Space Administration) and published by . This book was released on 1961 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made in the Langley Unitary Plan wind tunnel to determine the behavior of paraglider models at moderate to high supersonic speeds. The models were deployed from a sting in the supersonic stream and steady-state aerodynamics performance data were obtained. Maximum values of the lift-drag ratio were about 1.4 at a Mach number of 2.65 and about 1.2 at a Mach number of 4.65. The angles of attack over which the models could be flown were limited by unsteady behavior of the canopy.

A Wind-tunnel Investigation at Subsonic and Low Supersonic Speeds of a Re-entry Vehicle with Retractable Wings

Download A Wind-tunnel Investigation at Subsonic and Low Supersonic Speeds of a Re-entry Vehicle with Retractable Wings PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 24 pages
Book Rating : 4.:/5 (31 download)

DOWNLOAD NOW!


Book Synopsis A Wind-tunnel Investigation at Subsonic and Low Supersonic Speeds of a Re-entry Vehicle with Retractable Wings by : Willard G. Smith

Download or read book A Wind-tunnel Investigation at Subsonic and Low Supersonic Speeds of a Re-entry Vehicle with Retractable Wings written by Willard G. Smith and published by . This book was released on 1961 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Note

Download NASA Technical Note PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 482 pages
Book Rating : 4.:/5 (319 download)

DOWNLOAD NOW!


Book Synopsis NASA Technical Note by :

Download or read book NASA Technical Note written by and published by . This book was released on 1966 with total page 482 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Wind-tunnel Investigation of Drag and Stabili- Ty of Parachutes at Supersonic Speeds

Download Wind-tunnel Investigation of Drag and Stabili- Ty of Parachutes at Supersonic Speeds PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 30 pages
Book Rating : 4.:/5 (317 download)

DOWNLOAD NOW!


Book Synopsis Wind-tunnel Investigation of Drag and Stabili- Ty of Parachutes at Supersonic Speeds by : Nickolai Charczenko

Download or read book Wind-tunnel Investigation of Drag and Stabili- Ty of Parachutes at Supersonic Speeds written by Nickolai Charczenko and published by . This book was released on 1964 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Preliminary Investigation of a Paraglider

Download Preliminary Investigation of a Paraglider PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.:/5 (31 download)

DOWNLOAD NOW!


Book Synopsis Preliminary Investigation of a Paraglider by : Francis Melvin Rogallo

Download or read book Preliminary Investigation of a Paraglider written by Francis Melvin Rogallo and published by . This book was released on 1960 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: A preliminary investigation of the aerodynamic and control characteristics of a flexible glider similar to a parachute in construction has been made at the Langley Research Center to evaluate its capabilities as a reentry glider. Preliminary weight estimates of the proposed vehicle indicate that such a structure can be made with extreamly low wing loading. Maximum temperatures during the reentry maneuver might be held as low as about 1,500 degrees F.

Wind Tunnel Investigation of Flexible Parachute Models at Supersonic Speeds

Download Wind Tunnel Investigation of Flexible Parachute Models at Supersonic Speeds PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 1 pages
Book Rating : 4.:/5 (227 download)

DOWNLOAD NOW!


Book Synopsis Wind Tunnel Investigation of Flexible Parachute Models at Supersonic Speeds by : L. A. MORGAN

Download or read book Wind Tunnel Investigation of Flexible Parachute Models at Supersonic Speeds written by L. A. MORGAN and published by . This book was released on 1962 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tests were conducted in the 40-in. Supersonic Tunnel of the von Karman Gas Dynamics Facility to determine the aerodynamic characteristics of a series of flexible parachute models at Mach numbers from 1.5 to 3. Parachutes of various designs employing porous, non-porous, and ribbon materials were tested by deployment from a modified Pershing model. High-speed movies and drag measurements were obtained. (Author).

Low-subsonic Wind-tunnel and Free-flight Drop-test Investigation of a Paraglider Configuration Having Large Tapered Leading Edges and Keel

Download Low-subsonic Wind-tunnel and Free-flight Drop-test Investigation of a Paraglider Configuration Having Large Tapered Leading Edges and Keel PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.:/5 (31 download)

DOWNLOAD NOW!


Book Synopsis Low-subsonic Wind-tunnel and Free-flight Drop-test Investigation of a Paraglider Configuration Having Large Tapered Leading Edges and Keel by : Delwin R. Croom

Download or read book Low-subsonic Wind-tunnel and Free-flight Drop-test Investigation of a Paraglider Configuration Having Large Tapered Leading Edges and Keel written by Delwin R. Croom and published by . This book was released on 1966 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Wind-tunnel Investigation at Subsonic and Supersonic Speeds of Static and Dynamic Stability Derivatives of Airplane Model with Unswept Wing and High Horizontal Tail [with List of References]

Download Wind-tunnel Investigation at Subsonic and Supersonic Speeds of Static and Dynamic Stability Derivatives of Airplane Model with Unswept Wing and High Horizontal Tail [with List of References] PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 77 pages
Book Rating : 4.:/5 (18 download)

DOWNLOAD NOW!


Book Synopsis Wind-tunnel Investigation at Subsonic and Supersonic Speeds of Static and Dynamic Stability Derivatives of Airplane Model with Unswept Wing and High Horizontal Tail [with List of References] by :

Download or read book Wind-tunnel Investigation at Subsonic and Supersonic Speeds of Static and Dynamic Stability Derivatives of Airplane Model with Unswept Wing and High Horizontal Tail [with List of References] written by and published by . This book was released on 1959 with total page 77 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The High-speed Flexible-throat Supersonic Wind Tunnel

Download The High-speed Flexible-throat Supersonic Wind Tunnel PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.3/5 (91 download)

DOWNLOAD NOW!


Book Synopsis The High-speed Flexible-throat Supersonic Wind Tunnel by :

Download or read book The High-speed Flexible-throat Supersonic Wind Tunnel written by and published by . This book was released on 1948 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Experimental and Theoretical Studies of the Effects of Camber and Twist on the Aerodynamic Characteristics of Parawings Having Normal Aspect Ratios of 3 and 6

Download Experimental and Theoretical Studies of the Effects of Camber and Twist on the Aerodynamic Characteristics of Parawings Having Normal Aspect Ratios of 3 and 6 PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 48 pages
Book Rating : 4.:/5 (31 download)

DOWNLOAD NOW!


Book Synopsis Experimental and Theoretical Studies of the Effects of Camber and Twist on the Aerodynamic Characteristics of Parawings Having Normal Aspect Ratios of 3 and 6 by : Edward Charles Polhamus

Download or read book Experimental and Theoretical Studies of the Effects of Camber and Twist on the Aerodynamic Characteristics of Parawings Having Normal Aspect Ratios of 3 and 6 written by Edward Charles Polhamus and published by . This book was released on 1963 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt: Low-speed wind-tunnel studies were made of the effects of camber and twist and the effects of aspect ratio on the aerodynamic characteristics of parawings. To determine the effects of camber and twist, tests were made both with the conventional conical-type canopy, which provides camber and washout, and with a cylindrical-type canopy which provides essentially zero camber and twist. With regard to aspect ratio, tests were made of parawings having aspect ratios of 3 and 6; the range was thereby extended well beyond that of previous investigations. The degree to which airfoil and wing theory can be used to predict the aerodynamic characteristics of parawings was also investigated.

NASA Scientific and Technical Reports

Download NASA Scientific and Technical Reports PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 2300 pages
Book Rating : 4.F/5 ( download)

DOWNLOAD NOW!


Book Synopsis NASA Scientific and Technical Reports by : United States. National Aeronautics and Space Administration Scientific and Technical Information Division

Download or read book NASA Scientific and Technical Reports written by United States. National Aeronautics and Space Administration Scientific and Technical Information Division and published by . This book was released on 1967 with total page 2300 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Large-scale Wind-tunnel Investigation of a Model with an External Jet-augmented Flap

Download Large-scale Wind-tunnel Investigation of a Model with an External Jet-augmented Flap PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (31 download)

DOWNLOAD NOW!


Book Synopsis Large-scale Wind-tunnel Investigation of a Model with an External Jet-augmented Flap by : Jerry V. Kirk

Download or read book Large-scale Wind-tunnel Investigation of a Model with an External Jet-augmented Flap written by Jerry V. Kirk and published by . This book was released on 1967 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Index of NASA Technical Publications

Download Index of NASA Technical Publications PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 448 pages
Book Rating : 4.:/5 (31 download)

DOWNLOAD NOW!


Book Synopsis Index of NASA Technical Publications by : United States. National Aeronautics and Space Administration

Download or read book Index of NASA Technical Publications written by United States. National Aeronautics and Space Administration and published by . This book was released on 1960 with total page 448 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Selected Listing of NASA Scientific and Technical Reports for ...

Download A Selected Listing of NASA Scientific and Technical Reports for ... PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 450 pages
Book Rating : 4.X/5 (4 download)

DOWNLOAD NOW!


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 1960 with total page 450 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Monthly Catalog of United States Government Publications, Cumulative Index

Download Monthly Catalog of United States Government Publications, Cumulative Index PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 1250 pages
Book Rating : 4.F/5 ( download)

DOWNLOAD NOW!


Book Synopsis Monthly Catalog of United States Government Publications, Cumulative Index by : United States. Superintendent of Documents

Download or read book Monthly Catalog of United States Government Publications, Cumulative Index written by United States. Superintendent of Documents and published by . This book was released on 1979 with total page 1250 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Monthly Catalog, United States Public Documents

Download Monthly Catalog, United States Public Documents PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 1716 pages
Book Rating : 4.E/5 ( download)

DOWNLOAD NOW!


Book Synopsis Monthly Catalog, United States Public Documents by : United States. Superintendent of Documents

Download or read book Monthly Catalog, United States Public Documents written by United States. Superintendent of Documents and published by . This book was released on 1968 with total page 1716 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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