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A Flight Determination of the Moments of the YG-1B Tapered Blade Rotor about the Hub Trunnions
Document ID: 20180002404
NTRS Full-Text: Click to View  [PDF Size: 5.2 MB]
Author: Bailey, F. J., Jr.
Abstract: At the request of the Materiel Division, Wright Field, the National Advisory Committee for hide
Publication Year: 1939
Document Type: Technical Report
Report/Patent Number: NACA-MR-X-1939
Date Acquired: Apr 23, 2018
Results of Landing Tests of Kellett YG-1 Autogiro (A. C. R. 35-278)
Document ID: 20180002405
NTRS Full-Text: Click to View  [PDF Size: 9.5 MB]
Author: Gilruth, R. R.
Abstract: Flight tests were made with a Kellett YG-1 autogiro to determine the relationship between the ground hide
Publication Year: 1937
Document Type: Technical Report
Report/Patent Number: NACA-MR-X-1937
Date Acquired: Apr 20, 2018
Blade Motion and Bouncing Tests of KD-1 Autogiro
Document ID: 20180002406
NTRS Full-Text: Click to View  [PDF Size: 17.4 MB]
Author: Wheatley, John B.
Abstract: There are forwarded herewith the results of blade motion and bouncing tests on the Kellett KD-1 hide
Publication Year: 1945
Document Type: Technical Report
Report/Patent Number: NACA-MR-X-1935
Date Acquired: Apr 17, 2018
Wire-Strain-Gage Hinge-Moment Indicators for Use in Tests of Airplane Models
Document ID: 20160011529
NTRS Full-Text: Click to View  [PDF Size: 10.8 MB]
Author: Edwards, Howard B.
Abstract: The design and construction of various forms of strain-gage spring units and hinge-moment assemblies hide
Publication Year: 1944
Document Type: Technical Report
Report/Patent Number: NACA-CB-L4D15
Date Acquired: Sep 28, 2016
Limitations of Lifting-Line Theory for Estimation of Aileron Hinge-Moment Characteristics
Document ID: 20160005146
Author: Swanson, Robert S.; Gillis, Clarence L.
Abstract: Hinge-moment parameters for several typical ailerons were calculated from section data with the hide
Publication Year: 1943
Document Type: Technical Report
Report/Patent Number: AD-A801563, NACA-WR-L-281, NACA-CB-3L02
Date Acquired: Apr 25, 2016
Spin-Tunnel Investigation of a 1/30-Scale Model of the North American A-5 Airplane
Document ID: 20160000758
NTRS Full-Text: Click to View  [PDF Size: 2.9 MB]
Author: Lee, Henry A.
Abstract: An investigation has been made to determine the erect and. inverted spin and recovery hide
Publication Year: 1964
Document Type: Technical Report
Report/Patent Number: NASA-TM-SX-946, NACA-AD-3140, L-3663
Date Acquired: Jan 15, 2016
Wings with Variable Camber and Slots
Document ID: 20150020405
NTRS Full-Text: Click to View  [PDF Size: 733 KB]
Author: Lacaine, J.
Abstract: Investigations with a view to increasing the lift coefficient of a wing, without greatly increasing hide
Publication Year: 1933
Document Type: Technical Report
Report/Patent Number: NACA Misc. Paper No. 37
Date Acquired: Nov 06, 2015
Preliminary Correlation of the Effects of Beveled Trailing Edges on the Hinge-Moment Characteristics of Control Surfaces
Document ID: 20150015606
NTRS Full-Text: Click to View  [PDF Size: 2.7 MB]
Author: Purser, Paul E.; Gillis, Clarence L.
Abstract: A study of available data from various tests of beveled control surfaces has been made in an attempt hide
Publication Year: 1943
Document Type: Technical Report
Report/Patent Number: NACA-CB-3E14
Date Acquired: Aug 28, 2015
Wind-Tunnel Tests of an NACA 44R-Series Tapered Wing with a Straight Trailing Edge and a Constant-Chord Center Section
Document ID: 20150013909
NTRS Full-Text: Click to View  [PDF Size: 1.4 MB]
Author: Neely, Robert H.
Abstract: As part of a general investigation in the NACA 19-foot pressure tunnel to determine stall hide
Publication Year: 1943
Document Type: Technical Report
Report/Patent Number: NACA RB No. 3L13
Date Acquired: Jul 23, 2015
Effects of Interaction Between Normal Shock and Boundary Layer
Document ID: 20140002003
NTRS Full-Text: Click to View  [PDF Size: 1.5 MB]
Author: Donaldson, Coleman duP.
Abstract: A discussion of the interaction between normal shocks and boundary layers on the basis of hide
Publication Year: 1944
Document Type: Technical Report
Report/Patent Number: NACA-CB-4A27
Date Acquired: Mar 19, 2014
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