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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Permanent Buckling Of Sheet-Stringer Panels At Elevated Temperatures
Author(s): Robert A. Needham Corporate Author: University Of California, Department Of Engineering Laboratory: Aircraft Laboratory Date of Publication: 1953-07 Report Number: WADC TR 53-209
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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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Effects of Spring and Inertia Devices on the Longitudinal Stability of Aircraft
Author(s): Joseph H. Goldberg Corporate Author: Princeton University Laboratory: Aircraft Laboratory Date of Publication: 1953-07 Report Number: WADC TR 53-350
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Method For Predicting Dynamic Landing Loads
Author(s): Richard L. Eisenman, Edward H. Kramer Corporate Author: Aircraft Laboratory Laboratory: Aircraft Laboratory Date of Publication: 1954-09 Report Number: WADC TR 54-28
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Subsonic Flutter Model Tests of Wings Carrying Heavy Tip Pods. Part 2. Swept Wings
Author(s): W. G. Brady; H. G. Maier; Walter T. Pargoff Corporate Author: Cornell Aeronautical Laboratory, Inc. Laboratory: Aircraft Laboratory Date of Publication: 1954-11 Report Number: WADC TR 53-161 Part 2
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A Study of Landing Gear Rebound and Subsequent Runout Characteristics
Author(s): L. T. Waterman; W. H. Sellers; C. W. Vickery; D. M. Kauffman Corporate Author: Fairchild Engine and Airplace Corporation Laboratory: Aircraft Laboratory Date of Publication: 1954-03 Report Number: WADC TR 54-110
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Indicial Downwash And Its Structural Effect On The Horizontal Tail
Author(s): Norman P. Hobbs Corporate Author: Massachusetts Institute Of Technology Laboratory: Aircraft Laboratory Date of Publication: 1956-08 Report Number: WADC TR 56-164
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Structural Design for Aerodynamic Heating Part III. Structural Design
Author(s): W. H. Dukes; A. Schintt Corporate Author: Bell Aircraft Corporation Laboratory: Aircraft Laboratory Date of Publication: 1955-10 Report Number: WADC TR 55-305 Part III
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Application Of The Variational Method, The Galerkin Technique, And Normal Coordinates In A Transient Temperature Distribution Problem
Author(s): L. A. Schmit Corporate Author: Massachusetts Institute Of Technology Laboratory: Aircraft Laboratory Date of Publication: 1956-09 Report Number: WADC TR 56-287
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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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Aerodynamic Ablation Of Melting Bodies
Author(s): Theodore R. Goodman Corporate Author: Allied Research Associates, Inc Laboratory: Aircraft Laboratory Date of Publication: 1957-10 Report Number: WADC TR 57-284
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Longitudinal Stability Investigation Of An F-100A Airplane
Author(s): Norman E. Gowin 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): Norman E. Gowin Corporate Author: Cornell Aeronautical Laboratory, Inc. Laboratory: Aircraft Laboratory Date of Publication: 1957-11 Report Number: WADC TR 57-563
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The Cumulative Effects Resulting From Repeated Irradiation Of A Simple Laboratory Specimen While Under The Influence Of A Static Uniform Bending Moment
Author(s): William J. Blackstock; John C. Loria Corporate Author: Massachusetts Institute Of Technology Laboratory: Aircraft Laboratory Date of Publication: 1957-07 Report Number: WADC TR 56-653
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Coiled Stainless Steel Tubing: Part II, Design Manual
Author(s): Ronald A Stouffer, James T. Hudson, Louis F. Freitag Corporate Author: Martin Company Laboratory: Aircraft Laboratory Date of Publication: 1957-12 Report Number: WADC TR 57-507 Part II
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Statistical Analysis of Experimental Measurements of Initial Conditions for Ground Landings
Author(s): Richard L. Eisenman; Nicholas A. Engler Corporate Author: Aircraft Laboratory; University of Dayton Laboratory: Aircraft Laboratory Date of Publication: 1956-03 Report Number: WADC TN 55-171 Volume II Appendix III
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Noise Transmission from Boundary Layer Pressure Fluctuations
Author(s): Robert H. Kraichnan Corporate Author: Columbia University Laboratory: Aircraft Laboratory Date of Publication: 1956-03 Report Number: WADC TN 56-263
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Statistical Analysis of Experimental Measurements of Initital Conditions for Ground Landings
Author(s): Richard L. Eisenman; Nicholas A. Engler Corporate Author: Aircraft Laboratory; University of Dayton Laboratory: Aircraft Laboratory Date of Publication: 1956-03 Report Number: WADC TN 55-171 Volume I
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Analytical Studies Of Aircraft Structures Exposed To Transient External Heating Summary Report Of Thermal Response Studies
Author(s): Takao Ishimoto Corporate Author: University of California, Department Of Engineering Laboratory: Aircraft Laboratory Date of Publication: 1958-06 Report Number: WADC TR 57-373
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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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An Experimental Investigation of the Flutter Characteristics of a Cusp-Type Spoiler
Author(s): R. H. Schwab and G. Fotieo Corporate Author: Glenn L. Martin Company Laboratory: Aircraft Laboratory Date of Publication: 1953-01 Report Number: AF TR 5785 AD Number:
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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
Flutter Tests of Large Straight Wing Models at High Subsonic Speeds
Author(s): White, Jr., Richard P. Corporate Author: Cornell Aeronautical Laboratory, Inc. Laboratory: Aircraft Laboratory Date of Publication: 1955-12 Report Number: WADC TR 55-334
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
Studies on Thermal Stresses for Aircraft Structures Exposed to Transient External Heating. Volume I. Evaluation of the Thermal Response, Force and Moment in a Plate.
Author(s): Mahlmeister, J. E. Corporate Author: University of California, Los Angeles, Department of Engineering Laboratory: Aircraft Laboratory Date of Publication: 1955-04 Report Number: WADC TR 55-192 Volume 1
Studies On Thermal Stresses For Aircraft Structures Exposed To Transient External Heating, Volume II. An Analytical Method For The Prediction Of Behavior Of A Sheet-Stringer Panel With A Uniformly Heated Surface
Author(s): Mahlmeister, J. E. Corporate Author: California U. Laboratory: Aircraft Laboratory Date of Publication: 1955-12 Report Number: WADC TR 55-192 Volume 2
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
Three-Dimensional Supersonic Flutter Model Tests Near Mach Number 1.5. Part II. Experimental And Theoretical Data For Bare wings And wings with Tip Tanks
Author(s): McCarthy Jr., John F. Corporate Author: Massachusetts Institute of Technology Laboratory: Aircraft Laboratory Date of Publication: 1955-12 Report Number: WADC TR 54-113 Part 2
An Experimental Investigation Of Hot Gas Ejectors For Boundary Layer Control
Author(s): Richard V. De Leo Corporate Author: Rosemount Aeronautical Laboratories, University of Minnesota Laboratory: Aircraft Laboratory Date of Publication: 1953-12 Report Number: WADC TR 52-128 Part 2
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Measurements with Honeycombs in the Full-Scale and in the Model Vertical Wind Tunnel
Author(s): Wilhem F. Knackstedt Corporate Author: Aircraft Laboratory Laboratory: Aircraft Laboratory Date of Publication: 1952-08 Report Number: WADC TR 52-207 AD Number: AD0008717
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Investigation of Discrepancies Between Flight-Measured and Calculated F-80A Derivatives and Respnonses Including a Study of Aeroelastic Effects
Author(s): Leonard Segel Corporate Author: Cornell Aeronautical Laboratory, Inc. Laboratory: Aircraft Laboratory Date of Publication: 1952-08 Report Number: WADC TR 52-130
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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
Three-dimensional Supersonic Flutter Model Tests Near Mach Number 1.5. Part 1: Model Design And Testing Techniques
Author(s): McCarthy, Jr., John F. Corporate Author: Aeroelastic And Structures Research Laboratory, Massachusetts Institute of Technology Laboratory: Aircraft Laboratory Date of Publication: 1955-12 Report Number: WADC TR 54-113 Part 1