106 reports
The Wall Pressure Distribution In A Choked Tunnel
Author(s): Guderley, Gottfried Corporate Author: Aircraft Laboratory Laboratory: Aircraft Laboratory Date of Publication: 1953-12 Report Number: WADC TR 53-509
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Principles of Canopy Design For Military Aircraft
Author(s): Nutt, Ambrose B. Corporate Author: Aircraft Laboratory Laboratory: Aircraft Laboratory Date of Publication: 1953-04 Report Number: WADC TR 53-92
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On The Flow Over A Finite Wedge In The Lower Transonic Region
Author(s): Yoshihara, Hideo Corporate Author: Aircraft Laboratory Laboratory: Aircraft Laboratory Date of Publication: 1956-06 Report Number: WADC TR 56-444
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Longitudinal Stability Investigation Of An F-100A Airplane
Author(s): Gowin, Norman E. Corporate Author: Cornell Aeronautical Laboratory, Inc. Laboratory: Aircraft Laboratory Date of Publication: 1957-11 Report Number: WADC TR 57-562
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Lateral Stability Investigation Of An F-100A Airplane
Author(s): Gowin, Norman E. Corporate Author: Cornell Aeronautical Laboratory, Inc. Laboratory: Aircraft Laboratory Date of Publication: 1957-11 Report Number: WADC TR 57-563
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Unsteady Airloads On Pointed Airfoils And Slender Bodies At High Mach Numbers
Author(s): Zartarian, Garabed Corporate Author: Aeroelastic And Structures Research Laboratory, Massachusetts Institute of Technology Laboratory: Aircraft Laboratory Date of Publication: 1959-12 Report Number: WADC TR 59-583
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Wing Weight Estimation
Author(s): Kelley, Joseph Laboratory: Aircraft Laboratory Date of Publication: 1944-11 Report Number: AAF TR 5161
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Flutter Model Tests Of A Swept-back, All-moving Horizontal Tail At Supersonic Speeds
Author(s): Asher, Gifford W. Corporate Author: Massachusetts Inst Of Tech Cambridge Laboratory: Aircraft Laboratory Date of Publication: 1957-11 Report Number: WADC TR 56-285
Soundproofing Materials and the Installation Thereof in Aircraft
Author(s): Grafman, A. J. Corporate Author: Frank Mayer Engineering Company Laboratory: Aircraft Laboratory Date of Publication: 1955-03 Report Number: WADC TR 55-97
Structural Design for Aerodynamic Heating. Part II. Analytical Studies
Author(s): Dukes, W. H. Corporate Author: Bell Aircraft Laboratory: Aircraft Laboratory Date of Publication: 1955-10 Report Number: WADC TR 55-305 Part 2
Coefficient of Friction of Aircraft Tires on Concrete Runways
Author(s): Luthman, Robert R. Corporate Author: University of Dayton Laboratory: Aircraft Laboratory Date of Publication: 1955-03 Report Number: WADC TR 55-179
Structural Design For Aerodynamic Heating. Part I: Design Information
Author(s): Dukes, W. H. Corporate Author: Bell Aircraft Corpoartion Laboratory: Aircraft Laboratory Date of Publication: 1955-10 Report Number: WADC TR 55-305 Part 1
Testing Of Metal Boss Seals
Author(s): Kupiec, Harry P. Corporate Author: Aircraft Equipment Testing Co. Laboratory: Aircraft Laboratory Date of Publication: 1955-04 Report Number: WADC TR 55-163
The Effect of an Axially Symmetric Fuselage on the Nonstationary Supersonic Airloads Acting on a Wing with Supersonic Edges
Author(s): Epstein, Melvin Corporate Author: Aircraft Laboratory Laboratory: Aircraft Laboratory Date of Publication: 1954-05 Report Number: WADC TR 54-196
Analytical Studies Of Aircraft Structures Exposed To Transient External Heating Volume IV Heat-Transfer Coefficients For Speeds Up To M-3, With Emphasis On Effects Of Wall-Temperature Variations
Author(s): Knuth, Eldon L. Corporate Author: University 0f California, Department Of Engineering Laboratory: Aircraft Laboratory Date of Publication: 1957-09 Report Number: WADC TR 54-579 Volume 4
Analytical Studies Of Aircraft Structures Exposed To Transient External Heating Volume III Thermal Response Of The Skin And Support Flange Of A Structural Joint
Author(s): Ambrosio, Alphonso Corporate Author: University 0f California, Department Of Engineering Laboratory: Aircraft Laboratory Date of Publication: 1955-01 Report Number: WADC TR 54-579 Volume 3
Shock-Tube Flow Investigations. Part 1. An Exploratory Study Of The Generation Of Blast -Type Profiles In The Shock Tube By The Reflection Method
Author(s): Lee, Robert C. K. Corporate Author: Massachusetts Institute Of Technology Laboratory: Aircraft Laboratory Date of Publication: 1956-08 Report Number: WADC TR 54-383 Part 1
Three-dimensional Supersonic Flutter Model Tests Near Mach Number 1.5. Part 3: Experimental and Theoretical Data for Wings with Control Surfaces
Author(s): Asher, Gifford W. Corporate Author: Massachusetts Institute of Technology Laboratory: Aircraft Laboratory Date of Publication: 1958-01 Report Number: WADC TR 54-113 Part 3
Subsonic Flow Over a Body Between Porous Walls
Author(s): Kassner, Rudolph R. Corporate Author: Wright Air Development Center Laboratory: Aircraft Laboratory Date of Publication: 1952-02 Report Number: WADC TR 52-9
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Analytical Studies Of Aircraft Structures Exposed To Transient External Heating. Vol. II: Thermal Response Of A Finite Plate And The "thin" Plate Criterion
Author(s): Ambrosio, Alphonso Corporate Author: University Of California, Department Of Engineering Laboratory: Aircraft Laboratory Date of Publication: 1954-11 Report Number: WADC TR 54-579 Volume 2
Analytical Studies Of Aircraft Structures Exposd To Transient External Heating Volume I Thermal Response Of A "Thin" Plate Under Influence Of A Constant Temperature Edge
Author(s): Ambrosio, Alphonso Corporate Author: University Of California, Department Of Engineering Laboratory: Aircraft Laboratory Date of Publication: 1954-05 Report Number: WADC TR 54-579 Volume 1
The Effects Of Thermal Radiation On Aircraft Structures, Part I. The M.I.T. Mark I Radiant Heating Structural Test Facility
Author(s): Loria, John C. Corporate Author: Massachusetts Institute Of Technology Laboratory: Aircraft Laboratory Date of Publication: 1954-10 Report Number: WADC TR 54-384 Part 1
Effects Of Structural Flexibility On Gust Loading Of Aircraft Part I: Gust Loads On Swept-wing Airplanes Free To Pitch And To Deform Statically
Author(s): Foss, K. A. Corporate Author: Peroelastic And Structures Research Laboratory, Massachusetts Institute Of Technology Laboratory: Aircraft Laboratory Date of Publication: 1955-03 Report Number: WADC TR 54-592 Part 1
Effects Of Structural Flexibility On Gust Loading Of Aircraft Part II: Dynamic Stresses In Swept-wing Airplanes
Author(s): Kirsch, A. A. Corporate Author: Peroelastic And Structures Research Laboratory, Massachusetts Institute Of Technology Laboratory: Aircraft Laboratory Date of Publication: 1955-08 Report Number: WADC TR 54-592 Part 2
The Effects Of Thermal Radiation On Aircraft Structures, Part 3. Structural Behavior Of Box-Beams Under Combined Static And Thermal Loads
Author(s): Loria, John C. Corporate Author: Massachusetts Institute Of Technology Laboratory: Aircraft Laboratory Date of Publication: 1957-06 Report Number: WADC TR 54-384 Part 3
Development Of Equipment For The Experimental Measurement Of The Moments Of Inertia, And Product Of Inertia Of Aircraft
Author(s): Woodward, Claude R. Corporate Author: Cornell Aeronautical Laboratory, Inc. Laboratory: Aircraft Laboratory Date of Publication: 1954-06 Report Number: WADC TR 54-237
Flutter Characteristics Of Low Aspect Ratio wings In Incompressible Flow. Part I: Development Of The Basic Theory Of The Method
Author(s): Lawrence, H. R. Corporate Author: Cornell Aeronautical Laboratory, Inc. Laboratory: Aircraft Laboratory Date of Publication: 1957-05 Report Number: WADC TR 54-412 Part 1
Theoretical Investigation Of Optimum Pressures In Aircraft Hydraulic Systems
Author(s): Cooke, Conrad H. Corporate Author: Glenn L. Martin Company Laboratory: Aircraft Laboratory Date of Publication: 1954-01 Report Number: WADC TR 54-189 Volume 2
Theoretical Investigation Of Optimum Pressures In Aircraft Hydraulic Systems
Author(s): Cooke, Conrad H. Corporate Author: Glenn L. Martin Company Laboratory: Aircraft Laboratory Date of Publication: 1954-01 Report Number: WADC TR 54-189 Volume 1
Evaluation of Traveling-Gust Method for Airfoils in Strong Blast Waves by Shock-Tube Tests
Author(s): Ruetenik, J. Ray Corporate Author: Massachusetts Institute of Technology Laboratory: Aircraft Laboratory Date of Publication: 1960-05 Report Number: WADD TR 60-279
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New Standard Atmosphere: The WADC 1952 Model Atmosphere
Author(s): Williams, D. T. Corporate Author: Aircraft Laboratory Laboratory: Aircraft Laboratory Date of Publication: 1954-03 Report Number: WADC TR 54-215
An Investigation Of The Experimental Determination Of Aircraft Inertia
Author(s): Woodard, Claude R. Corporate Author: Cornell Aeronautical Laboratory, Inc. Laboratory: Aircraft Laboratory Date of Publication: 1953-07 Report Number: WADC TR 53-207
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Aerodynamic Noise And The Estimation Of Noise In Aircraft
Author(s): Rogers, Orville R. Corporate Author: Aircraft Laboratory Laboratory: Aircraft Laboratory Date of Publication: 1952-02 Report Number: WADC TR 52-341 AD Number: AD0013026
Investigation Of Methods For The Retention Of Air Frame Control Bearings In Structural Housings
Author(s): Asch, Abraham B. Corporate Author: Asch Equipment Company Laboratory: Aircraft Laboratory Date of Publication: 1957-01 Report Number: WADC TR 56-502
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Temp-Tapes: Improved Design, Construction, And Calibration
Author(s): Ambrosio, Alphonso Corporate Author: University Of California, Department Of Engineering Laboratory: Aircraft Laboratory Date of Publication: 1953-07 Report Number: WADC TR 53-211
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Thermal Response Of A Thin Plate With Radiation Losses
Author(s): Ambrosio, Alphonso Corporate Author: Dept. Of Engineering, University of California Laboratory: Aircraft Laboratory Date of Publication: 1958-06 Report Number: WADC TR 56-212
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Temperature Distributions In A Typical Aircraft Structure Due To Transient External Heating, Volume I, T-33 Airplane
Author(s): Ambrosio, Alphonso Corporate Author: University Of California, Department Of Engineering, Los Angeles, California Laboratory: Aircraft Laboratory Date of Publication: 1953-04 Report Number: WADC TR 52-216
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Boundary Layer Control On 64A006 And 64A010 Airfoils At High Subsonic Speeds
Author(s): Leadon, B. M. Corporate Author: Dept. Of Aeronautical Engineering, University Of Minnesota Laboratory: Aircraft Laboratory Date of Publication: 1953-10 Report Number: WADC TR 53-490
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Mehtods For Predicting Aeroelastic Effects On Subsonic Static Longitudinal Stability Of Aircraft
Author(s): Paraghamian, B. Corporate Author: Dept. Of Aerodynamics, Martin Company Laboratory: Aircraft Laboratory Date of Publication: 1954-09 Report Number: WADC TR 54-265
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Thermo-Elastic Stresses And Deflections In Beam-Columns
Author(s): Boley, Bruno A. Corporate Author: Institute Of Air Flight Structures, Columbia University Laboratory: Aircraft Laboratory Date of Publication: 1954-03 Report Number: WADC TR 54-425
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Thermo-Elastic Stresses And Deflections In Thin-Walled Beams
Author(s): Boley, Bruno A. Corporate Author: Institute Of Flight Structures, Columbia University Laboratory: Aircraft Laboratory Date of Publication: 1954-12 Report Number: WADC TR 54-426
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Thermal Stress Analysis For Aircraft Structures Part II. Bibliography
Author(s): Boley, Bruno A. Corporate Author: Institute Of Flight Structures, Department Of Civil Engineering and Engineering Mechanics, Columbia University. Laboratory: Aircraft Laboratory Date of Publication: 1955-11 Report Number: WADC TR 56-102 Part 2
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Thermal Stress Analysis For Aircraft Structures Theory And Methods Of Analysis
Author(s): Boley, Bruno A. Corporate Author: Institute Of Flight Structures, Columbia University. Laboratory: Aircraft Laboratory Date of Publication: 1955-08 Report Number: WADC TR 56-102 Part 1
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Experimental Studies On The Postfailure Response Of A Simple Structural Model Subjected To Static And Dynamic Loading
Author(s): D'Amato, Richard Corporate Author: Massachusetts Institute Of Technology Laboratory: Aircraft Laboratory Date of Publication: 1956-11-15 Report Number: WADC TR 56-161
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Improving Fatigue Life Of Fromed Stainless Steel Hydraulic Tubing By Prestressing
Author(s): Yen, C. S. Corporate Author: Douglas Aircraft Company, Inc. Laboratory: Aircraft Laboratory Date of Publication: 1956-05 Report Number: WADC TR 56-120
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Rolling Effectiveness and Aileron Reversal Characteristics of Straight and Sweptback Wings: Part 3. Evaluation and Test Results
Author(s): Groth, Eric Corporate Author: Aircraft Laboratory Laboratory: Aircraft Laboratory Date of Publication: 1952-09 Report Number: AF TR 6198 Part 3 AD Number: AD0003719
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Evaluation Of High Temperature Hydraulic Seals To Temperature Of 550 Degrees F. Part I: Mechanical Evealuation
Author(s): Galloway, Charles W. Corporate Author: Santa Monica Division, Douglas Aircraft Company, Inc. Laboratory: Aircraft Laboratory Date of Publication: 1958-02 Report Number: WADC TR 57-76 Part 1
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Study Of Coiled Tubing For Aircraft Hydraulic Systems
Author(s): Cooke, Conrad H. Corporate Author: Glenn L. Martin Company Laboratory: Aircraft Laboratory Date of Publication: 1955-02 Report Number: WADC TR 55-121
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Aeroelastic Effects On Dynamic Longitudinal Stability
Author(s): Goland, Martin Corporate Author: Midwest Research Inst Kansas City MO Laboratory: Aircraft Laboratory Date of Publication: 1953-07 Report Number: WADC TR 53-29
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Wind Tunnel Tests of the Coanda Wing and Nozzle
Author(s): Young, D. W. Corporate Author: Aircraft Laboratory Laboratory: Aircraft Laboratory Date of Publication: 1950-09 Report Number: AF TR 6199
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