A Comparison of the Lateral Controllability with Flap and Plug Ailerons on a Sweptback-wing Model Having Full-span Flaps

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ISBN 13 :
Total Pages : 30 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis A Comparison of the Lateral Controllability with Flap and Plug Ailerons on a Sweptback-wing Model Having Full-span Flaps by : Powell M. Lovell

Download or read book A Comparison of the Lateral Controllability with Flap and Plug Ailerons on a Sweptback-wing Model Having Full-span Flaps written by Powell M. Lovell and published by . This book was released on 1950 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt: A free-flight-tunnel investigation has been made to compare the dynamic lateral control characteristics provided by step plug ailerons on a sweptback-wing model having full-span flaps. The model had a 38 degree sweptback wing with an aspect ratio of 3 and a taper ratio of 0.05. The static stability and control characteristics of the flight-test model were determined from force tests and the time-lag characteristics of the ailerons were determined from stand tests in which there was freedom only in roll. Flight tests of the model were made over a range of lift coefficient from 1.0 through the stall.

A Comparison of the Lateral Controllability with Flap and Plug Ailerons on a Sweptback-wing Model Having Full-span Flaps

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Total Pages : pages
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Book Synopsis A Comparison of the Lateral Controllability with Flap and Plug Ailerons on a Sweptback-wing Model Having Full-span Flaps by : Powell M Lovell (Jr)

Download or read book A Comparison of the Lateral Controllability with Flap and Plug Ailerons on a Sweptback-wing Model Having Full-span Flaps written by Powell M Lovell (Jr) and published by . This book was released on 1950 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Index of NACA Technical Publications

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ISBN 13 :
Total Pages : 498 pages
Book Rating : 4.:/5 (2 download)

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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 1952 with total page 498 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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

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ISBN 13 :
Total Pages : 750 pages
Book Rating : 4.X/5 (4 download)

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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 750 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Comparison of the Lateral Controllability With Flap and Plug Ailerons on a Sweptback-Wing Model

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ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis A Comparison of the Lateral Controllability With Flap and Plug Ailerons on a Sweptback-Wing Model by :

Download or read book A Comparison of the Lateral Controllability With Flap and Plug Ailerons on a Sweptback-Wing Model written by and published by . This book was released on 1950 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been conducted to compare the dynamic lateral control characteristics provided by step plug ailerons with those provided by conventional flap ailerons on a sweptback-wing model. The model used had a 38c sweptback wing with an aspect ratio of 3 and a taper ratio of O.5. The static stability and control characteristics of the flight test model were determined from force tests and the lag characteristics of the ailerons were determined from roll-free stand tests. Flight tests of the model were made through a range of lift coefficient from 0.6 through the stall by using the data obtained from the force tests to establish the flight test conditions. At each lift coefficient in the flight test range the flap ailerons were adjusted to produce the same static rolling moment as was obtained by maximum projection of the plug ailerons. The controllability of the model was more satisfactory with plug ailerons alone than with flap ailerons alone except at lift coefficients below about 0.7. At the lower lift coefficients the time lag from full control deflection to maximum rolling acceleration caused by the plug ailerons was more objectionable than the slight adverse yawing caused by the flap ailerons; whereas, at the higher lift coefficients, the loss of rolling effectiveness caused by the large adverse yawing moments of the flap ailerons was more objectionable than the lag of the plug ailerons. At the stall, the model could be controlled satisfactorily with the plug ailerons alone or with the flap ailerons and rudder but could not be controlled satisfactorily with the flap ailerons alone.

Annual Report of the National Advisory Committee for Aeronautics

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ISBN 13 :
Total Pages : 1200 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Annual Report of the National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics

Download or read book Annual Report of the National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1954 with total page 1200 pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.

Technical Note - National Advisory Committee for Aeronautics

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ISBN 13 :
Total Pages : 856 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis Technical Note - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics

Download or read book Technical Note - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1950 with total page 856 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Stress and Distortion Analysis of a Swept Box Beam Having Bulkheads Perpendicular to the Spars

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ISBN 13 :
Total Pages : 712 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Stress and Distortion Analysis of a Swept Box Beam Having Bulkheads Perpendicular to the Spars by : Richard R. Heldenfels

Download or read book Stress and Distortion Analysis of a Swept Box Beam Having Bulkheads Perpendicular to the Spars written by Richard R. Heldenfels and published by . This book was released on 1950 with total page 712 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method is presented for the approximate calculation of the stresses and distortions in a box beam representing the main structural component of a swept wing with a carry-through section and with bulkheads perpendicular to the spars. The application of the method is illustrated by a numerical example and its results are compared with previously published test data.

List of Technical Notes, 1947-1953

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ISBN 13 :
Total Pages : 162 pages
Book Rating : 4.0/5 ( download)

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Book Synopsis List of Technical Notes, 1947-1953 by : United States. National Advisory Committee for Aeronautics

Download or read book List of Technical Notes, 1947-1953 written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1954 with total page 162 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Monthly Catalog of United States Government Publications

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ISBN 13 :
Total Pages : 1376 pages
Book Rating : 4.3/5 (121 download)

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Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 1951 with total page 1376 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Collection of Technical Papers on Guidance and Control

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ISBN 13 :
Total Pages : 848 pages
Book Rating : 4.:/5 (318 download)

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Download or read book Collection of Technical Papers on Guidance and Control written by and published by . This book was released on 1974 with total page 848 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Report

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ISBN 13 :
Total Pages : 620 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Report by :

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:

Report - National Advisory Committee for Aeronautics

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ISBN 13 :
Total Pages : 996 pages
Book Rating : 4.E/5 ( download)

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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 1950 with total page 996 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Report

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Total Pages : pages
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Book Synopsis Report by :

Download or read book Report written by and published by . This book was released on 1952 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Applied Mechanics Reviews

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ISBN 13 :
Total Pages : 810 pages
Book Rating : 4.F/5 ( download)

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Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1952 with total page 810 pages. Available in PDF, EPUB and Kindle. Book excerpt:

ESDU Engineering Sciences Data

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ISBN 13 :
Total Pages : 256 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis ESDU Engineering Sciences Data by :

Download or read book ESDU Engineering Sciences Data written by and published by . This book was released on 1991 with total page 256 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aircraft Stability and Control

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Publisher : Elsevier Science & Technology
ISBN 13 :
Total Pages : 710 pages
Book Rating : 4.:/5 (318 download)

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Book Synopsis Aircraft Stability and Control by : A. W. Babister

Download or read book Aircraft Stability and Control written by A. W. Babister and published by Elsevier Science & Technology. This book was released on 1961 with total page 710 pages. Available in PDF, EPUB and Kindle. Book excerpt: