Effect of Winglets on a First-generation Jet Transport Wing. 6: Stability Characteristics for a Full-span Model at Subsonic Speeds

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Total Pages : 74 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Effect of Winglets on a First-generation Jet Transport Wing. 6: Stability Characteristics for a Full-span Model at Subsonic Speeds by : Stuart G. Flechner

Download or read book Effect of Winglets on a First-generation Jet Transport Wing. 6: Stability Characteristics for a Full-span Model at Subsonic Speeds written by Stuart G. Flechner and published by . This book was released on 1979 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Experimental Results of Winglets on First, Second, and Third Generation Jet Transports

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ISBN 13 :
Total Pages : 24 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Experimental Results of Winglets on First, Second, and Third Generation Jet Transports by : Stuart G. Flechner

Download or read book Experimental Results of Winglets on First, Second, and Third Generation Jet Transports written by Stuart G. Flechner and published by . This book was released on 1978 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Experimental Results of Winglets on First, Second, and Third Generation Jet Transports

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ISBN 13 :
Total Pages : 26 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Experimental Results of Winglets on First, Second, and Third Generation Jet Transports by : Stuart G. Fletcher

Download or read book Experimental Results of Winglets on First, Second, and Third Generation Jet Transports written by Stuart G. Fletcher and published by . This book was released on 1978 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 996 pages
Book Rating : 4.3/5 (91 download)

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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 1978 with total page 996 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

NASA Technical Paper

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ISBN 13 :
Total Pages : 136 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis NASA Technical Paper by :

Download or read book NASA Technical Paper written by and published by . This book was released on 1986 with total page 136 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Scientific and Technical Publications

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ISBN 13 :
Total Pages : 410 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis NASA Scientific and Technical Publications by :

Download or read book NASA Scientific and Technical Publications written by and published by . This book was released on 1987 with total page 410 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Memorandum

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ISBN 13 :
Total Pages : 388 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis NASA Technical Memorandum by :

Download or read book NASA Technical Memorandum written by and published by . This book was released on 1981 with total page 388 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Reference Publication

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ISBN 13 :
Total Pages : 770 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis NASA Reference Publication by :

Download or read book NASA Reference Publication written by and published by . This book was released on 1977 with total page 770 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effect of Winglets on a First-generation Jet Transport Wing. 5: Stability Characteristics of a Full-span Wing with a Generalized Fuselage at High Subsonic Speeds

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ISBN 13 :
Total Pages : 76 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Effect of Winglets on a First-generation Jet Transport Wing. 5: Stability Characteristics of a Full-span Wing with a Generalized Fuselage at High Subsonic Speeds by : Peter F. Jacobs

Download or read book Effect of Winglets on a First-generation Jet Transport Wing. 5: Stability Characteristics of a Full-span Wing with a Generalized Fuselage at High Subsonic Speeds written by Peter F. Jacobs and published by . This book was released on 1978 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt: The effects of winglets on the static aerodynamic stability characteristics of a KC-135A jet transport model at high subsonic speeds are presented. The investigation was conducted in the Langley 8 foot transonic pressure tunnel using 0.035-scale wing panels mounted on a generalized research fuselage. Data were taken over a Mach number range from 0.50 to 0.95 at angles of attack ranging from -12 deg to 20 deg and sideslip angles of 0 deg, 5 deg, and -5 deg. The model was tested at two Reynolds number ranges to achieve a wide angle of attack range and to determine the effect of Reynolds number on stability. Results indicate that adding the winglets to the basic wing configuration produces small increases in both lateral and longitudinal aerodynamic stability and that the model stability increases slightly with Reynolds number. The winglets do increase the wing bending moments slightly, but the buffet onset characteristics of the model are not affected by the winglets.

Effects of Winglets on a First-generation Jet Transport Wing

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ISBN 13 :
Total Pages : 64 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Effects of Winglets on a First-generation Jet Transport Wing by : Robert R. Meyer (Jr.)

Download or read book Effects of Winglets on a First-generation Jet Transport Wing written by Robert R. Meyer (Jr.) and published by . This book was released on 1986 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt: "The effect of sideslip on winglet loads and selected wing loads was investigated at high and low subsonic Mach numbers. The investigation was conducted in two separate wind tunnel facilities, using two slightly different 0.035-scale full-span models. Results are presented which indicate that, in general, winglet loads as a result of sideslip are analogous to wing loads caused by angle of attack. The center-of-pressure locations on the winglets are somewhat different than might be expected for an analogous wing. The spanwise center of pressure for a winglet tends to be more inboard than for a wing. The most notable chordwise location is a forward center-of-pressure location on the winglet at high sideslip angles. The noted differences between a winglet and an analogous wing are the result of the influence of the wing on the winglet."--Technical report documentation page.

Effects of Winglets on a First-generation Jet Transport Wing. 7: Sideslip Effects on Winglet Loads and Selected Wing Loads at Subsonic Speeds for a Full-span Model

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Total Pages : 64 pages
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Book Synopsis Effects of Winglets on a First-generation Jet Transport Wing. 7: Sideslip Effects on Winglet Loads and Selected Wing Loads at Subsonic Speeds for a Full-span Model by : Robert R. Jr Meyer

Download or read book Effects of Winglets on a First-generation Jet Transport Wing. 7: Sideslip Effects on Winglet Loads and Selected Wing Loads at Subsonic Speeds for a Full-span Model written by Robert R. Jr Meyer and published by . This book was released on 1986 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA SP.

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ISBN 13 :
Total Pages : 396 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis NASA SP. by :

Download or read book NASA SP. written by and published by . This book was released on 1962 with total page 396 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effect of an Alternate Winglet on the Pressure and Spanwise Load Distributions of a First-generation Jet Transport Wing

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ISBN 13 :
Total Pages : 102 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Effect of an Alternate Winglet on the Pressure and Spanwise Load Distributions of a First-generation Jet Transport Wing by : Lawrence C. Montoya

Download or read book Effect of an Alternate Winglet on the Pressure and Spanwise Load Distributions of a First-generation Jet Transport Wing written by Lawrence C. Montoya and published by . This book was released on 1978 with total page 102 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Monthly Catalog of United States Government Publications

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ISBN 13 :
Total Pages : 1320 pages
Book Rating : 4.3/5 (121 download)

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Book Synopsis Monthly Catalog of United States Government Publications by :

Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 1978 with total page 1320 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Monthly Catalogue, United States Public Documents

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ISBN 13 :
Total Pages : 2248 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Monthly Catalogue, United States Public Documents by :

Download or read book Monthly Catalogue, United States Public Documents written by and published by . This book was released on 1978 with total page 2248 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effects of Winglets on First-generation Jet Transport Wing

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ISBN 13 :
Total Pages : 102 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Effects of Winglets on First-generation Jet Transport Wing by : Peter F. Jacobs

Download or read book Effects of Winglets on First-generation Jet Transport Wing written by Peter F. Jacobs and published by . This book was released on 1978 with total page 102 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aeronautical Engineering

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ISBN 13 :
Total Pages : 592 pages
Book Rating : 4.3/5 ( download)

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Book Synopsis Aeronautical Engineering by :

Download or read book Aeronautical Engineering written by and published by . This book was released on 1985 with total page 592 pages. Available in PDF, EPUB and Kindle. Book excerpt: A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).