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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
Nomenclature for Aeronautics
Document ID: 20100021420
NTRS Full-Text: Click to View  [PDF Size: 21.0 MB]
Abstract: The nomenclature for aeronautics presented in this Report No. 474 is a revision of the last previous hide
Publication Year: 1939
Document Type: Reprint
Report/Patent Number: NACA-TR-474
Date Acquired: Jun 14, 2010
Evaluation of Gust and Draft Velocities from Flights of P-61C Airplanes within Thunderstorms July 24, 1946 to August 6, 1946 at Orlando, Florida
Document ID: 20090035616
NTRS Full-Text: Click to View  [PDF Size: 1.7 MB]
Author: Tolefson, Harold B.
Abstract: The results obtained from gust and draft velocity measurements within thunderstorms for the period hide
Publication Year: 1947
Document Type: Technical Report
Report/Patent Number: NACA-RM-L7C28
Date Acquired: Oct 07, 2009
Paths of Target Seeking Missiles in Two Dimensions
Document ID: 20090033671
NTRS Full-Text: Click to View  [PDF Size: 11.1 MB]
External Online Source:

Author: Watkins, Charles E.
Abstract: Parameters that enter into equation of trajectory of a missile are discussed. Investigation is made hide
Publication Year: 1946
Document Type: Technical Report
Report/Patent Number: AD-A800542, NACA-ACR-L6B06, ATI No. 4831
Date Acquired: Sep 22, 2009
Cooling of Gas Turbines. 2; Effectiveness of Rim Cooling of Blades
Document ID: 20090033674
NTRS Full-Text: Click to View  [PDF Size: 19.6 MB]
External Online Source:

Author: Wolfenstein, Lincoln; Meyer, Gene L.; McCarthy, John S.
Abstract: An analysis of rim cooling, which cools the blade by condition alone, was conducted. Gas hide
Publication Year: 1945
Document Type: Technical Report
Report/Patent Number: AD-A800637, NACA-MR-E5I20
Date Acquired: Sep 22, 2009
Effect of a Leading-edge Flap upon the Lift, Drag, and Pitching Moment of an Airplane Employing a Thin, Unswept Wing
Document ID: 20090032234
NTRS Full-Text: Click to View  [PDF Size: 977 KB]
Author: Heitmeyer, John C.
Abstract: The effects of deflecting full-span, constant-chord, leading-edge flaps, having either round or hide
Publication Year: 1954
Document Type: Technical Report
Report/Patent Number: NACA-RM-SA54B16
Date Acquired: Sep 14, 2009
Force Characteristics in the Submerged and Planing Condition of a 1/5.78-Scale Model of a Hydro-Ski-Wheel Combination for the Grumman JRF-5 Airplane. TED No. NACA DE 357
Document ID: 20090026574
NTRS Full-Text: Click to View  [PDF Size: 3.0 MB]
Author: Land, Norman S.; Pelz, Charles A.
Abstract: Force characteristics determined from tank tests of a 1/5.78 scale model of a hydro-ski-wheel hide
Publication Year: 1952
Document Type: Technical Report
Report/Patent Number: NACA-RM-SLS2B28
Date Acquired: Aug 03, 2009
Wind-Tunnel Investigation of a 1/5-Scale Model of the Ryan XF2R Airplane
Document ID: 20090026606
NTRS Full-Text: Click to View  [PDF Size: 14.7 MB]
Author: Wong, Park Y.
Abstract: Wind-tunnel tests on a 1/5-scale model of the Ryan XF2R airplane were conducted to determine the hide
Publication Year: 1947
Document Type: Technical Report
Report/Patent Number: NACA-Rm-SA7E26
Date Acquired: Aug 03, 2009
An Investigation of the McDonnell XP-85 Airplane in the Ames 40- by 80-foot Wind Tunnel. Force and Moment Tests
Document ID: 20090026988
NTRS Full-Text: Click to View  [PDF Size: 155.9 MB]
Author: Hunton, Lynn W.; James Harry A.
Abstract: Wind-tunnel tests of the McDonnell XP-85 airplane were conducted to determine its longitudinal, hide
Publication Year: 1948
Document Type: Technical Report
Report/Patent Number: NACA-RM-SA8I23
Date Acquired: Aug 03, 2009
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