69 reports
Investigation of Certain Unsteady Aerodynamic Effects in Longitudinal Dynamic Stability
Author(s): H. Ashley; G. Zartarian; D. O. Neilson Corporate Author: Massachusetts Institute of Technology Laboratory: Aircraft Laboratory Date of Publication: 1951-12 Report Number: AF TR 5986
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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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Flight Test Investigation to Determine the Effectiveness of a Rocket as an Emergency Spin Recovery Device
Author(s): G. H. Farmer; B. G. Peterson Corporate Author: North American Aviation, Inc. Laboratory: Aircraft Laboratory Date of Publication: 1952-01 Report Number: WADC TR 52-233
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Rolling Effectiveness and Aileron Reversal Characteristics of Straight and Sweptback Wings: Part 3. Evaluation and Test Results
Author(s): Eric Groth 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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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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Boundary Layer Control On 64A006 And 64A010 Airfoils At High Subsonic Speeds
Author(s): B. M. Leadon, G. E. Anderson 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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The Wall Pressure Distribution In A Choked Tunnel
Author(s): Gottfried Guderley Corporate Author: Aircraft Laboratory Laboratory: Aircraft Laboratory Date of Publication: 1953-12 Report Number: WADC TR 53-509
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Temperature Distributions In A Typical Aircraft Structure Due To Transient External Heating, Volume I, T-33 Airplane
Author(s): Alphonso Ambrosio; Bertram Bussell; William F. Macinnes 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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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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Temp-Tapes: Improved Design, Construction, And Calibration
Author(s): Alphonso Ambrosio; Bertram Busseli 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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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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Principles of Canopy Design For Military Aircraft
Author(s): Ambrose B. Nutt Corporate Author: Aircraft Laboratory Laboratory: Aircraft Laboratory Date of Publication: 1953-04 Report Number: WADC TR 53-92
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Aeroelastic Effects On Dynamic Longitudinal Stability
Author(s): Goland, Martin; Luke, Yudell L. 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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Flight Test Investigation to Determine the Effectiveness of a Rocket as an Emergency Spin Recovery Device: Phase II
Author(s): G. H. Farmer Corporate Author: North American Aviation, Inc. Laboratory: Aircraft Laboratory Date of Publication: 1953-08 Report Number: WADC TR 53-396
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Effects of Airplane Elasticity and Unsteady Flow on Longitudinal Stability
Author(s): Martin Goland; Tudell L. Luke; Irving Sacks Corporate Author: Midwest Research Institute Laboratory: Aircraft Laboratory Date of Publication: 1953-11 Report Number: WADC TR 53-425
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Design Manual for Determining the Thermal Characteristics of High Speed Aircraft
Author(s): H. A. Johnson; M. W. Rubesin; F. M. Sauer; E. G. Slack; L. Possner Corporate Author: University of California, Berkeley Laboratory: Aircraft Laboratory Date of Publication: 1947-09-10 Report Number: AF TR 5632
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Thermoelastic Stresses In Beams
Author(s): Euval S. Barrekette Corporate Author: Institute of Flight Structures; Columbia University Laboratory: Aircraft Laboratory Date of Publication: 1950-02 Report Number: WADC TR 59-178
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Wind Tunnel Tests of the Coanda Wing and Nozzle
Author(s): D. W. Young; D. Zonars Corporate Author: Aircraft Laboratory Laboratory: Aircraft Laboratory Date of Publication: 1950-09 Report Number: AF TR 6199
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An Investigation Of The Experimental Determination Of Aircraft Inertia
Author(s): Claude R. Woodard Corporate Author: Cornell Aeronautical Laboratory, Inc. Laboratory: Aircraft Laboratory Date of Publication: 1953-07 Report Number: WADC TR 53-207
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Thermo-Elastic Stresses And Deflections In Beam-Columns
Author(s): Bruno A. Boley; Harold Mechanic 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): Bruno A. Boley; Irwin S. Tolins 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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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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Study Of Coiled Tubing For Aircraft Hydraulic Systems
Author(s): Conrad H. Cooke; Ronald D. Stouffer Corporate Author: Glenn L. Martin Company Laboratory: Aircraft Laboratory Date of Publication: 1955-02 Report Number: WADC TR 55-121
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Theoretical Studies of the Effects of Aspect Ratio on Flutter
Author(s): Martin Goland; Y. L. Luke; M. A. Dengler Corporate Author: Midwest Research Institute Laboratory: Aircraft Laboratory Date of Publication: 1954-06 Report Number: WADC TR 54-29
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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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Thermal Stress Analysis For Aircraft Structures Theory And Methods Of Analysis
Author(s): Bruno A.Boley,Jerome H.Weiner And Irwin S. Tolins 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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Destruction Tests Of Aircraft Structural Components; Part 2. Development Of A Single-Channel Bending Moment Measurement Method Applicable To A Complex Built-Up Structure For Both The Elastic And The Post-Buckling Regime Of Structural Response
Author(s): Emanuel S. Criscione; Mi Hran Ayvazian; Kenneth R. Wetmore Corporate Author: Massachusetts Institute Of Technology Laboratory: Aircraft Laboratory Date of Publication: 1955-09 Report Number: WADC TR 54-385 Part 2
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A Method For The Approximate Solution Of The Heat Equation
Author(s): Jerome H. Weiner Corporate Author: Institute Of Flight Structures,Columbia University Laboratory: Aircraft Laboratory Date of Publication: 1955-03 Report Number: WADC TR 54-427
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Thermal Stress Analysis For Aircraft Structures Part II. Bibliography
Author(s): Bruno A.Boley And Jerome H.Weiner 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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Improving Fatigue Life Of Fromed Stainless Steel Hydraulic Tubing By Prestressing
Author(s): C. S. Yen, B. V. Whiteson Corporate Author: Douglas Aircraft Company, Inc. Laboratory: Aircraft Laboratory Date of Publication: 1956-05 Report Number: WADC TR 56-120
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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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The Temperature Response Of Thick Plates Exposed To Radiant Heat Pulses
Author(s): John C. Loria And Lucien A. Schmit Corporate Author: Massachusetts Institute Of Technology Laboratory: Aircraft Laboratory Date of Publication: 1956-07-25 Report Number: WADC TR 56-149
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Development of a One-Piece Plastic Windshield for High-Speed Aircraft
Author(s): Rolland D. Huff; Stanley C. Patrick; Charles R. Frownfelter Corporate Author: Goodyear Aircraft Corporation Laboratory: Aircraft Laboratory Date of Publication: 1955-06 Report Number: WADC TN 55-241 Part I
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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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Experimental Studies On The Postfailure Response Of A Simple Structural Model Subjected To Static And Dynamic Loading
Author(s): Richard D' Amato 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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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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Ejection Seat Tests Conducted On The 10,000 Foot Aerodynamic Research Track At Edwards Air Force Base
Author(s): Hodell, C. K.; Rosner, A. H. Corporate Author: Air Force Flight Dynamics Lab Wright-Patterson AFB OH Laboratory: Aircraft Laboratory Date of Publication: 1957-11 Report Number: WADC TR 52-63
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Thermal Stresses In Free Plates Under Heat Pulse Inputs
Author(s): Jerome H. Weiner; Harold Mechanic Corporate Author: Institute Of Air Flight Structures, Columbia University Laboratory: Aircraft Laboratory Date of Publication: 1957-03 Report Number: WADC TR 54-428
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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 I. Test Results
Author(s): Joseph J. Chmura, Jr. , Ronald D. Stouffer, Albert N. Winter Corporate Author: Martin Company Laboratory: Aircraft Laboratory Date of Publication: 1957-07 Report Number: WADC TR 57-507 Part I
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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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Investigation Of Hydraulic Low Friction Teflon Cap Seals
Author(s): John O. Bruno Corporate Author: Hydra-Power Corporation Laboratory: Aircraft Laboratory Date of Publication: 1957-12 Report Number: WADC TR 57-163
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Investigation Of Methods For The Retention Of Air Frame Control Bearings In Structural Housings
Author(s): Abraham B. Asch Corporate Author: Asch Equipment Company Laboratory: Aircraft Laboratory Date of Publication: 1957-01 Report Number: WADC TR 56-502
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Synthetic Mica High Temperature Strain Gage Research
Author(s): Given A. Brewer Corporate Author: Brewer Engineering Laboratories Laboratory: Aircraft Laboratory Date of Publication: 1957-12 Report Number: WADC TR 57-306
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Evaluation Of High Temperature Hydraulic Seals To Temperature Of 550 Degrees F. Part I: Mechanical Evealuation
Author(s): Charles W. Galloway 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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Management Briefing on Low Drag Boundary Layer Control
Author(s): Joseph Flatt; Richard H. Klepinger Corporate Author: Aircraft Laboratory Laboratory: Aircraft Laboratory Date of Publication: 1956-11-08 Report Number: WADC TR 56-662
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