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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
Column and Plate Compressive Strength of Extruded XB75S-T Aluminum Alloy
Document ID: 20140000276
NTRS Full-Text: Click to View  [PDF Size: 4.6 MB]
Author: Heimerl, George J.; Roy, J. Albert
Abstract: Results are presented of tests to determine the column and plate compressive strength of extruded hide
Publication Year: 1944
Document Type: Technical Report
Report/Patent Number: NACA RB No. L4E26
Date Acquired: Jan 17, 2014
A Concise Theoretical Method for Profile-Drag Calculation; Advance Report
Document ID: 20110020378
NTRS Full-Text: Click to View  [PDF Size: 1.2 MB]
Author: Nitzberg, Gerald E.
Abstract: In this report a method is presented for the calculation of the profile drag of airfoil sections. hide
Publication Year: 1944
Document Type: Technical Report
Report/Patent Number: NACA ACR No. 4B05
Date Acquired: Nov 03, 2011
Wind-Tunnel Tests of a Portion of a PV-2 Helicopter Rotor Blade
Document ID: 20100027413
NTRS Full-Text: Click to View  [PDF Size: 1.6 MB]
Author: Kemp, William B., Jr.
Abstract: A portion of a PV-2 helicopter rotor blade has been tested in the 6- by 6-foot test section of the hide
Publication Year: 1945
Document Type: Technical Report
Report/Patent Number: NACA-MR-L5C29b
Date Acquired: Aug 06, 2010
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