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Wagner Eugene H (26 results)
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Condition: As New. Unread book in perfect condition.
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Pamphlet. Condition: Very Good. Staple bound paperback in very good condition. Underlining on some pages. Other than that, all inside pages are in great shape. Minor shelf wear to the cover. 24 pages. Measures 7 x 4.2 inches.
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Condition: As New. Unread book in perfect condition.
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An Analytical Study of T-38 Drag Reduction in Tight Formation Flight
Seller: GreatBookPricesUK, Woodford Green, United Kingdom
Seller rating 5 out of 5 stars
US$ 26.98
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An Analytical Study of T-38 Drag Reduction in Tight Formation Flight
Seller: GreatBookPricesUK, Woodford Green, United Kingdom
Seller rating 5 out of 5 stars
US$ 31.57
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Add to basketCondition: As New. Unread book in perfect condition.
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An Analytical Study of T-38 Drag Reduction in Tight Formation Flight
Seller: GreatBookPricesUK, Woodford Green, United Kingdom
Seller rating 5 out of 5 stars
US$ 40.11
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An Analytical Study of T-38 Drag Reduction in Tight Formation Flight
Seller: GreatBookPricesUK, Woodford Green, United Kingdom
Seller rating 5 out of 5 stars
US$ 47.03
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Theory of Strength of Materials. Memos No. 800, 809, 854, 658 (Technical Memorandums, National Advisory Committee for Aeronautics)
Published by Washington: National Advisory Committee for Aeronautics
Hardcover. Condition: Good. Hardcover. Blue cloth over boards. "Theory of Strength of Materials" written on the spine in white paint, with a square of white paint further down the spine. Measures 10.5 x 8 inches. Multiple sections bound together in library binding; each section individually paginated. Sections are numbered as follows: 800, 809, 854, and 658 -- published, respectively, in 1936, 1936, 1938, and 1938. The first section is titled "Charts for Checking the Stability of Compression Members in Trusses". 21 pages. The next is titled "Tests for the Determination of the Stress Condition in Tension Fields". 13 pages. Section 3 is titled "Twisting of Thin Walled Columns Perfectly Restrained at One End". 17 pages. The last section, "Generalized Analysis of Experimental Observations in Problems of Elastic Stability", is 13 pages. Each section is followed by multiple figures and tables. The entire volume, with original covers, has a later library binding. Gutters at front and back reinforced with white cloth. Two library stamps and an inscription in pen on the front free endpaper. Pages within are clean and free of foreign markings. Light rubbing to covers. Comes from a large collection of technical memorandums from the National Advisory Committee for Aeronautics before the committee was abolished upon creation of NASA in 1958. Be sure to check our other listings for the rest of the collection.
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An Analytical Study of T-38 Drag Reduction in Tight Formation Flight
Language: English
Published by Creative Media Partners, LLC, 2025
ISBN 10: 1025131789 ISBN 13: 9781025131788
PAP. Condition: New. New Book. Shipped from UK. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.
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An Analytical Study of T-38 Drag Reduction in Tight Formation Flight
Language: English
Published by Creative Media Partners, LLC Mai 2025, 2025
ISBN 10: 1025131789 ISBN 13: 9781025131788
Taschenbuch. Condition: Neu. Neuware.
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An Analytical Study of T-38 Drag Reduction in Tight Formation Flight
Language: English
Published by Creative Media Partners, LLC Mai 2025, 2025
ISBN 10: 1025128702 ISBN 13: 9781025128702
Buch. Condition: Neu. Neuware.
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An Analytical Study of T-38 Drag Reduction in Tight Formation Flight
Language: English
Published by Creative Media Partners, LLC, 2025
ISBN 10: 1025131789 ISBN 13: 9781025131788
Seller: PBShop.store UK, Fairford, GLOS, United Kingdom
Seller rating 5 out of 5 stars
US$ 22.47
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Add to basketPAP. Condition: New. New Book. Delivered from our UK warehouse in 4 to 14 business days. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.
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US$ 101.13
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Add to basketPaperback. Condition: Like New. Like New. book.
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Condition: New. Print on Demand.
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An Analytical Study of T-38 Drag Reduction in Tight Formation Flight
Language: English
Published by Creative Media Partners, LLC, 2025
ISBN 10: 1025128702 ISBN 13: 9781025128702
HRD. Condition: New. New Book. Shipped from UK. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.
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Condition: New. Print on Demand.
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An Analytical Study of T-38 Drag Reduction in Tight Formation Flight
Language: English
Published by Creative Media Partners, LLC, 2025
ISBN 10: 1025128702 ISBN 13: 9781025128702
Seller: PBShop.store UK, Fairford, GLOS, United Kingdom
Seller rating 5 out of 5 stars
US$ 36.40
US$ 5.60 shipping
Ships from United Kingdom to U.S.A.Quantity: Over 20 available
Add to basketHRD. Condition: New. New Book. Delivered from our UK warehouse in 4 to 14 business days. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.
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Condition: New. PRINT ON DEMAND.
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30 Hefte: Der arme Vetter, Die Richterin, Gustav Adolfs Page, Der eingebildete Kranke, Prinz Friedrich von Homburg, Die Wildente, Der Richter von Zalamea, Die Feuerprobe, Parsifal, Tristan und Isolde, Rienzi, Des Lebens Überfluss, Robinson soll nicht sterben, Der Heiratsvermittler, Die Judenbuche, Dr. med. Hiob Prätoris, Brigitta, Antigone, Das Lied der Gottheit, Agnes Bernauer, Julius Cäsar, Pole Poppenspäler, Minna von Barnhelm, Reden des Buddha, Die deutschen Kleinstädter, Die schwarze Spinne, Wo ist Onkel Bertram, Das Glas Wasser oder Ursachen und Wirkungen, Elisabeth von England, Gedichte
Published by Reclam, Stuttgart, verschiedene Jahrgänge
Seller: Versandantiquariat Kerzemichel, Wittenberge, Germany
Seller rating 5 out of 5 stars
Einbände leicht berieben,Krt, Rücken leicht eingerissen, Einbände und Kopfschnitt leicht nachgedunkelt, sonst gute Exemplare.
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Condition: New. Print on Demand.
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Condition: New. Print on Demand.
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Condition: New. PRINT ON DEMAND.
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US$ 26.99
US$ 49.76 shipping
Ships from United Kingdom to U.S.A.Quantity: 1 available
Add to basketPaperback. Condition: new. Paperback. This thesis explores the benefits of flying in a tight formation, mimicking the natural behavior of migratory birds such as geese. The first phase of the research was to determine an optimal position for the wingman of a tight formation flight of T-38 Talon aircraft using the HASC95 vortex lattice code. A second wingman was then added to determine the benefit derived by increasing formation size. The second wingman was predicted to derive an even greater induced drag benefit than the first wingman for T-38s operating at Mach 0.54 at a 10,000-foot altitude. The predicted values were 17.5% savings for the second wingman versus 15% for the first wingman. The flight test phase flew two and three-ship formations to validate the computational work. The results of the two-ship flight tests showed with 80% confidence that the wingman saved fuel in the predicted optimal position (86% wingspan lateral spacing). This position yielded actual fuel savings of 8.8% 5.0% versus the predicted 15%. The other lateral positions did not show a statistically significant fuel savings. The flight test team felt that the three-ship formation data was inconclusive due to the difficulty of trying to fly a stable position as the third aircraft in the formation without station-keeping ability.This work has been selected by scholars as being culturally important, and is part of the knowledge base of civilization as we know it. This work was reproduced from the original artifact, and remains as true to the original work as possible. Therefore, you will see the original copyright references, library stamps (as most of these works have been housed in our most important libraries around the world), and other notations in the work.This work is in the public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work.As a reproduction of a historical artifact, this work may contain missing or blurred pages, poor pictures, errant marks, etc. Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant. This item is printed on demand. Shipping may be from our UK warehouse or from our Australian or US warehouses, depending on stock availability.
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US$ 40.85
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Ships from United Kingdom to U.S.A.Quantity: 1 available
Add to basketHardcover. Condition: new. Hardcover. This thesis explores the benefits of flying in a tight formation, mimicking the natural behavior of migratory birds such as geese. The first phase of the research was to determine an optimal position for the wingman of a tight formation flight of T-38 Talon aircraft using the HASC95 vortex lattice code. A second wingman was then added to determine the benefit derived by increasing formation size. The second wingman was predicted to derive an even greater induced drag benefit than the first wingman for T-38s operating at Mach 0.54 at a 10,000-foot altitude. The predicted values were 17.5% savings for the second wingman versus 15% for the first wingman. The flight test phase flew two and three-ship formations to validate the computational work. The results of the two-ship flight tests showed with 80% confidence that the wingman saved fuel in the predicted optimal position (86% wingspan lateral spacing). This position yielded actual fuel savings of 8.8% 5.0% versus the predicted 15%. The other lateral positions did not show a statistically significant fuel savings. The flight test team felt that the three-ship formation data was inconclusive due to the difficulty of trying to fly a stable position as the third aircraft in the formation without station-keeping ability.This work has been selected by scholars as being culturally important, and is part of the knowledge base of civilization as we know it. This work was reproduced from the original artifact, and remains as true to the original work as possible. Therefore, you will see the original copyright references, library stamps (as most of these works have been housed in our most important libraries around the world), and other notations in the work.This work is in the public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work.As a reproduction of a historical artifact, this work may contain missing or blurred pages, poor pictures, errant marks, etc. Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant. This item is printed on demand. Shipping may be from our UK warehouse or from our Australian or US warehouses, depending on stock availability.
