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Aerodynamics

 Subject

Staff Only
Subject Source: Library of Congress Subject Headings

Found in 94 Collections and/or Records:

"Interference Effects of Single and Multiple Round or Slotted Jets on a VTOL Model in Transition" (NASA Technical Note TN D-2380), 1964-08

 Item — Box MC-019-002, Folder: 001.A.056
Identifier: 20060043
Scope and Contents

Document Type: Technical Research Report. Purpose: Authoritative reference Authority: Government Civil Document Number: NASA Technical Note TN D-2380, dated August 1964.

Scope: Preliminary NASA research report by Raymond D. Vogler of Langley Research Center, Langley Station, Hampton, Va.

Contents: See title.

Dates: Publication: 1964-08
Found in: The University of Alabama in Huntsville Archives & Special Collections / Aircraft Engine Historical Society Collection / Series I: Aeronautical Research, Development, Test & Evaluation (RDT & E) / Sub-series I.A: Aircraft RDT&E

Introduction to Aerodynamics of a Compressible Fluid, 1947, 1947

 Item — Special collection MC-19, Book: 047, Call No.: TL 574 .C4 L5
Identifier: 20061121
Scope and Contents Document Type: Book (Technical)Purpose: Authoritative Reference.Authority: Author Expertise.Series: Galcit Aeronautical SeriesScope (from Author's Preface): "The subject, Aerodynamics of Compressible Fluids, has been studied at great length by both pure mathematicians and "practical" engineers, and the literature on the subject has become extensive. The material presented in this book is designed to furnish the reader...
Dates: Copyright: 1947; Publication: 1947
Found in: The University of Alabama in Huntsville Archives & Special Collections / Aircraft Engine Historical Society Collection / Series I: Aeronautical Research, Development, Test & Evaluation (RDT & E) / Sub-series I.E: Aeronautical RDT&E (Special Collection)

"Investigation in the Langley 19-Foot Pressure Tunnel of Two Wings of NACA 65-210 and 64-210 Airfoil Sections with Various Type Flaps" (NACA Report No. 942), 1949

 Item — Box MC-019-001, Folder: 001.A.026
Identifier: 20060147
Scope and Contents

Document Type: Technical Research Report. Authority: Government Civil (authoritative reference). Document Number: National Advisory Committee for Aeronautics (NACA) Report No. 942, published in 1949.

Scope: NACA research report by James C. Sivells and Stanley H. Spooner.

Contents: See title.

Dates: Publication: 1949
Found in: The University of Alabama in Huntsville Archives & Special Collections / Aircraft Engine Historical Society Collection / Series I: Aeronautical Research, Development, Test & Evaluation (RDT & E) / Sub-series I.A: Aircraft RDT&E

"Investigation of A Semispan Tilting-Propeller Configuration and Effects of Ratio of Wing Cord to Propeller Diameter on Several Small-Cord Tilting-Wing Configurations at Transitions Speeds" (NASA Technical Note TN D-1815), 1963-07

 Item — Box MC-019-002, Folder: 001.A.051
Identifier: 20060026
Scope and Contents

Document Type: Technical Research Report. Purpose: Authoritative reference Authority: Government Civil Document Number: NASA Technical Note TN D-1815, dated July 1963.

Scope: Preliminary NASA research report by Kenneth P. Spreemann of Langley Research Center, Langley Station, Hampton, Va.

Contents: See title.

Dates: Publication: 1963-07
Found in: The University of Alabama in Huntsville Archives & Special Collections / Aircraft Engine Historical Society Collection / Series I: Aeronautical Research, Development, Test & Evaluation (RDT & E) / Sub-series I.A: Aircraft RDT&E

"Investigation of Separation of the Turbulent Boundary Layer" (NACA Report 1030), 1951

 Item — Box MC-019-001, Folder: 001.A.027
Identifier: 20060150
Scope and Contents

Document Type: Technical Research Report. Authority: Government Civil (authoritative reference). Document Number: National Advisory Committee for Aeronautics (NACA) Report No. 1030, published in 1951.

Scope: Research report by G. B. Schubauer and P. S. Klebanoff of the United States National Bureau of Standards, with funding provided by NACA.

Contents: See title.

Dates: Publication: 1951
Found in: The University of Alabama in Huntsville Archives & Special Collections / Aircraft Engine Historical Society Collection / Series I: Aeronautical Research, Development, Test & Evaluation (RDT & E) / Sub-series I.A: Aircraft RDT&E

"Lift and Drag of Wings with Small Span" [Translation of paper titled "Auftrieb und Widerstand des Tragflügels kleiner Spannweite" by F. Weinig] (NACA Technical Memorandum No. 1151), 1942-09-08, 1947-08

 Item — Box MC-019-002, Folder: 001.A.039
Identifier: 20060160
Scope and Contents Document Type: Technical Research Report (Translation). Purpose: Authoritative reference Authority: Government Civil Document Number: NACA Technical Memorandum No.1151, dated August 1947. Originally published as Deutsche Luftfahrtforschung Forschungsbericht [German Aviation Research Report] Nr. 1665 (dated September 8, 1942 in Stuttgart) by Zentrale für wissenschaftliches Berichtswesen der Luftfahrtforschung des Generalluftzeugmeisters (ZWB) Berlin-Adlershof.Scope: Translation of...
Dates: Publication: 1942-09-08; Issued: 1947-08
Found in: The University of Alabama in Huntsville Archives & Special Collections / Aircraft Engine Historical Society Collection / Series I: Aeronautical Research, Development, Test & Evaluation (RDT & E) / Sub-series I.A: Aircraft RDT&E

"Low-Subsonic Measurements of Static and Dynamic Stability Derivatives of Six Flat-Plate Wings Having Leading -Edge Sweep Angles of 70 degrees To 84 degrees" (NASA Technical Note TN D-1822), 1963-07

 Item — Box MC-019-002, Folder: 001.A.051
Identifier: 20060027
Scope and Contents

Document Type: Technical Research Report. Purpose: Authoritative reference Authority: Government Civil Document Number: NASA Technical Note TN D-1822, dated July 1963.

Scope: Preliminary NASA research report by Robert E. Shanks of Langley Research Center, Langley Station, Hampton, Va.

Contents: See title.

Dates: Publication: 1963-07
Found in: The University of Alabama in Huntsville Archives & Special Collections / Aircraft Engine Historical Society Collection / Series I: Aeronautical Research, Development, Test & Evaluation (RDT & E) / Sub-series I.A: Aircraft RDT&E

"Method for Calculating the Rolling and Yawing Moments due to Rolling for Unswept Wings With or Without Flaps or Ailerons By Use of Nonlinear Section Lift Data" (NACA Report 1167), 1954

 Item — Box MC-019-001, Folder: 001.A.028
Identifier: 20060154
Scope and Contents

Document Type: Technical Research Report. Authority: Government Civil (authoritative reference). Document Number: National Advisory Committee for Aeronautics (NACA) Report No. 1167, published in 1954.

Scope: NACA research report by Albert P. Martina.

Contents: See title.

Dates: Publication: 1954
Found in: The University of Alabama in Huntsville Archives & Special Collections / Aircraft Engine Historical Society Collection / Series I: Aeronautical Research, Development, Test & Evaluation (RDT & E) / Sub-series I.A: Aircraft RDT&E

"Numerical Predictions of Nonlinear Diffusion with Homogeneous Recombination and Time-Varying Boundary Conditions" (NASA Technical Note TN D-2126), 1964-01

 Item — Box MC-019-002, Folder: 001.A.053
Identifier: 20060033
Scope and Contents

Document Type: Technical Research Report. Purpose: Authoritative reference Authority: Government Civil Document Number: NASA Technical Note TN D-2126, dated January 1964.

Scope: Preliminary NASA research report by Walter A. Reinhardt of Ames Research Center, Moffett Field, Calif.

Contents: See title

Dates: Publication: 1964-01
Found in: The University of Alabama in Huntsville Archives & Special Collections / Aircraft Engine Historical Society Collection / Series I: Aeronautical Research, Development, Test & Evaluation (RDT & E) / Sub-series I.A: Aircraft RDT&E

"Parasite Resistance Variables with Incidence" (Bulletin of the Airplane Engineering Department, U.S.A, Vol. I, No. 2), 1918-07

 Item — Box MC-019-001, Folder: 001.A.002
Identifier: 20140702
Scope and Contents Document Type: Technical Research Report Authority: Government Military (authoritative reference) Document Number: Bulletin of the Airplane Engineering Department, U.S.A. [United States Army], Vol. I, No. 2 (dated July 1918. This section on pages 140 through 141.Scope: Report by Aeronautical Research Department. Intended for limited, controlled distribution (see General note on publication data).Contents: article includes "Wind Tunnel Tests Show Errors in Performance...
Dates: Publication: 1918-07
Found in: The University of Alabama in Huntsville Archives & Special Collections / Aircraft Engine Historical Society Collection / Series I: Aeronautical Research, Development, Test & Evaluation (RDT & E) / Sub-series I.A: Aircraft RDT&E

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