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Determination Of The Stability And Control Characteristics Of A Tailless All Wing Airplane Model With Sweepback In The Langley Free Flight Tunnel
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Book Synopsis Determination of the Stability and Control Characteristics of a Tailless All-wing Airplane Model with Sweepback in the Langley Free-flight Tunnel by : John P. Campbell
Download or read book Determination of the Stability and Control Characteristics of a Tailless All-wing Airplane Model with Sweepback in the Langley Free-flight Tunnel written by John P. Campbell and published by . This book was released on 1945 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: Summary: An investigation to determine the power-off stability and control characteristics of a tailless all-wing airplane model with sweepback has been made in the Langley free-flight tunnel. The results of the free-flight tunnel tests were correlated with results from force tests made at high Reynolds numbers in order to estimate the flying characteristics of the full-scale airplane. The investigation consisted of force and flight tests of a 4.3-foot-span dynamic model. The effects of flap deflection, center-of-gravity location, and addition of vertical-tail area were determined. The following conclusions were drawn from the results of the investigation: The full-sale airplane will undergo a serious reduction in stick-fixed longitudinal stability at high life coefficients unless early wing-tip stalling is eliminated. The directional stability of an all-wing airplane without vertical tail surfaces will be undesirably low. The effective dihedral of an airplane of this type should be kept low. An elevon and rudder control system similar to that used on this design should provide sufficient control.
Book Synopsis Determination of the Stability and Control Characteristics of a Tailless All-wing Airplane Model With Sweepback in the Langley Free-flight Tunnel by : Langley Aeronautical Laboratory
Download or read book Determination of the Stability and Control Characteristics of a Tailless All-wing Airplane Model With Sweepback in the Langley Free-flight Tunnel written by Langley Aeronautical Laboratory and published by Hassell Street Press. This book was released on 2021-09-09 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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 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. Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. To ensure a quality reading experience, this work has been proofread and republished using a format that seamlessly blends the original graphical elements with text in an easy-to-read typeface. We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant.
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 1955 with total page 242 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 1949 with total page 664 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Index of NACA Reports Having Application to Personal Aircraft by : United States. National Advisory Committee for Aeronautics
Download or read book Index of NACA Reports Having Application to Personal Aircraft written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1946 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wartime Report Release List by : United States. National Advisory Committee for Aeronautics
Download or read book Wartime Report Release List written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1947 with total page 200 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis NACA Wartime Report by : United States. National Advisory Committee for Aeronautics
Download or read book NACA Wartime Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on with total page 730 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wartime Report written by and published by . This book was released on with total page 282 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wartime Report by : United States. National Advisory Committee for Aeronautics
Download or read book Wartime Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on with total page 300 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Determination of the Stability and Control Characteristics of a Straight-wing, Tailless Fighter-airplane Model in the Langley Free-flight Tunnel by : Charles L. Seacord
Download or read book Determination of the Stability and Control Characteristics of a Straight-wing, Tailless Fighter-airplane Model in the Langley Free-flight Tunnel written by Charles L. Seacord and published by . This book was released on 1946 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt: Summary: An investigation to determine the stability and control characteristics of a straight-wing, tailless fighter model with a pusher propeller designed by the NACA has been made in the Langley free-flight tunnel. The investigation consisted principally of force and flight tests of a powered dynamic model. The effects of tail configuration, center-of-gravity location, and power on the stability and control characteristics of the model were determined. Tests were also made in the Langley 15-foot free-spinning tunnel to determine whether the model would trim at very high angles of attack.
Book Synopsis Determination of the Stability and Control Characteristics of a Straigth-wing, Tailless Fighter-airplane Model in the Langley Free-flight Tunnel by : Charles L. Seacord
Download or read book Determination of the Stability and Control Characteristics of a Straigth-wing, Tailless Fighter-airplane Model in the Langley Free-flight Tunnel written by Charles L. Seacord and published by . This book was released on 1946 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Report - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics
Download or read book Report - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1947 with total page 652 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Annual Report - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics
Download or read book Annual Report - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1955 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Download or read book Report written by and published by . This book was released on 1945 with total page 620 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Bibliography of Scientific and Industrial Reports by :
Download or read book Bibliography of Scientific and Industrial Reports written by and published by . This book was released on 1949 with total page 608 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Tailless Aircraft Performance Improvements with Relaxed Static Stability by :
Download or read book Tailless Aircraft Performance Improvements with Relaxed Static Stability written by and published by . This book was released on 1989 with total page 146 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Determination of the Stability and Control Characteristics of a Straight-wing, Tailless Fighter-airplane Model in the Langley Free-flight Tunnel by : Charles L. Jr Seacord
Download or read book Determination of the Stability and Control Characteristics of a Straight-wing, Tailless Fighter-airplane Model in the Langley Free-flight Tunnel written by Charles L. Jr Seacord and published by . This book was released on 1946 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
