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A Technique for Measuring In-Plane Displacements By Holographic Interferometry
Report Number: AFFDL TR 72-5
Author(s): Frank D. Adams; Richard R. Corwin
Corporate Author: Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 2/1/1972
Pages: 30
Contract: Laboratory Research - No Contract
Project: 1467
Task: 146702
AD Number: AD0744490
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Conceptual Studies of Aerodynamic Glider-Decelerator Combinations for Heavy Loads
Report Number: AFFDL TR 72-6
Author(s): Heinrich, Helmut G.; Saari, David P.
Corporate Author: Minnesota Univ Minneapolis Dept Of Aerospace Engineering And Mechanics
Publication Date: 5/1/1972
Pages: 48
Project: 0
Task: 0
AD Number: AD0902633
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Recent Notes and Data on Interference Heating
Report Number: AFFDL TR 72-12
Author(s): Neumann,Richard D.
Corporate Author: Air Force Flight Dynamics Lab Wright-Patterson AFB Ohio
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 2/1/1972
Pages: 38
Contract: Laboratory Research - No Contract
Project: 1366
Task: 136607
AD Number: AD0747765
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V/STOL Aircraft Aerodynamic Prediction Methods Investigation: Volume I. Theoretical Development of Prediction Methods
Report Number: AFFDL TR 72-26 Volume 1
Author(s): P. T. Wooler; H. C. Kao; M. F. Scwendemann; H. R. Wasson; H. Ziegler
Corporate Author: Northrop Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 1/1/1972
Pages: 238
Contract: F33615-69-C-1602
Project: 698BT
Task: None Given
AD Number: AD0752557
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V/STOL Aircraft Aerodynamic Prediction Methods Investigation: Volume II. Application of Prediction Methods
Report Number: AFFDL TR 72-26 Volume 2
Author(s): P. T. Wooler; H. C. Kao; M. F. Scwendemann; H. R. Wasson; H. Ziegler
Corporate Author: Northrop Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 1/1/1972
Pages: 250
Contract: F33615-69-C-1602
Project: 698BT
Task: None Given
AD Number: AD0752558
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V/STOL Aircraft Aerodynamic Prediction Methods Investigation: Volume III. Manual for Computer Programs
Report Number: AFFDL TR 72-26 Volume 3
Author(s): P. T. Wooler; H. C. Kao; M. F. Scwendemann; H. R. Wasson; H. Ziegler
Corporate Author: Northrop Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 1/1/1972
Pages: 206
Contract: F33615-69-C-1602
Project: 698BT
Task: None Given
AD Number: AD0752559
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V/STOL Aircraft Aerodynamic Prediction Methods Investigation: Volume IV. Literature Survey
Report Number: AFFDL TR 72-26 Volume 4
Author(s): P. T. Wooler; H. C. Kao; M. F. Scwendemann; H. R. Wasson; H. Ziegler
Corporate Author: Northrop Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 1/1/1972
Pages: 78
Contract: F33615-69-C-1602
Project: 698BT
Task: None Given
AD Number: AD0752563
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Response of Aircraft to Three Dimensional Random Turbulence
Report Number: AFFDL TR 72-28
Author(s): Frederick D. Eichenbaum
Corporate Author: Lockheed-Georgia Company
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 10/1/1972
Pages: 104
Contract: F33615-71-C-1878
Project: 1367
Task: 136702
AD Number: AD0756886
Photo Enhancement: Not Needed
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Evaluation of Lateral-Directional Handling Qualities and Roll-Sideslip Coupling of Fighter Class Airplanes
Report Number: AFFDL TR 72-36 Volume 1
Author(s): Boothe, Edward M.; Parrag, Michael L.
Corporate Author: Cornell Aeronautical Lab Inc Buffalo N Y
Laboratory: Flight Dynamics Laboratory
Publication Date: 5/1/1972
Pages: 152
Project: 0
Task: 0
AD Number: AD0748435
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Evaluation of Lateral-Directional Handling Qualities and Roll-Sideslip Coupling of Fighter Class Airplanes
Report Number: AFFDL TR 72-36 Volume 2
Author(s): Boothe, Edward M.; Parrag, Michael L
Corporate Author: Cornell Aeronautical Lab Inc Buffalo N Y
Laboratory: Flight Dynamics Laboratory
Publication Date: 5/1/1972
Pages: 224
Project: 0
Task: 0
AD Number: AD0748436
Photo Enhancement: Not Needed
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An Analysis of the Stability and Control Characteristics of an Ejector Wing V/STOL During Transition
Report Number: AFFDL TR 72-37
Author(s): George Kurylowich; James M. Martin
Corporate Author: Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 2/1/1973
Pages: 193
Contract: Laboratory Research - No Contract
Project: D095
Task: None Given
AD Number: AD0912045
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V/STOL Dynamics and Aeroelastic Rotor-Airfram Technology
Report Number: AFFDL TR 72-40 Volume 1
Author(s): H. R. Alexander; P. F. Leone
Corporate Author: The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 1/1/1973
Pages: 134
Contract: F33615-71-C-1310
Project: 1370
Task: 137005
AD Number: AD0908244
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V/STOL Dynamics and Aeroelastic Rotor - Airframe Technology. Volume II. Description and Correlation of New Methodologies.
Report Number: AFFDL TR 72-40 Volume 2
Author(s): Alexander, H. R.; Amos, A. K.; Tarzanin, F. J.; Taylor, R. B.
Corporate Author: Boeing Vertol Co Philadelphia PA
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 9/1/1972
Pages: 330
Contract: F33615-71-C-1310
Project: 1370
Task: 137005
AD Number: AD0904089
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V/STOL Dynamics and Aeroelastic Rotor-Airframe Technology. Volume III. User's Manuals - Computer Programs for Aeroelastic Stability Analysis and Aeroelastic Prop/Rotor Loads Analysis.
Report Number: AFFDL TR 72-40 Volume 3
Author(s): Amos, A. K. Tarzanin, F. J.
Corporate Author: Boeing Vertol Co Philadelphia PA
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 9/1/1972
Pages: 226
Contract: F33615-71-C-1310
Project: 1370
Task: 137005
AD Number: AD0904665
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Revisions to MIL-F-8785B (ASG) Proposed by Cornell Aeronautical Laboratory
Report Number: AFFDL TR 72-41
Author(s): Charles R. Chalk; Dante A. DiFranco; J. Victor Lebacqz; T. Peter Neal
Corporate Author: Calspan Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 4/1/1973
Pages: 484
Features: + Diagram(s) + Foldout(s) + Graph(s) + Table(s)
Contract: F33615-71-C-1254
Project: 8219
Task: 821905
AD Number: ADD453445
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Abstract Text:
In August 1969, the Air Force and the Naval Air Systems Command adopted MIL-F-8785B(ASG) as the official Military Specification for Flying Qualities of Piloted Airplanes. Since that time effort has been sponsored by the Air Force to further improve the specification document and to increase its applicability in the development of future weapons systems. Results of a study preformed by Calspan (formerly Cornell Aeronautical Laboratory) are presented in this report. Changes to the requirements of MIL-F-8785B(ASG) are suggested in the following areas:
1. Longitudinal maneuvering dynamics and control gradients.
2. Lateral-directional maneuvering dynamics and roll-sideslip coupling.
3. Atmospheric disturbance models.
4. Stall-spin characteristics.
5. Numerous miscellaneous corrections and changes.
6. Additions to Background Information and Users Guide for MIL-F-8785B(ASG).
Substantiation data for the recommended changes is also presented.
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MAGIC III: An Automated General Purpose System for Structural Analysis Volume 1. Engineer's Manual.
Report Number: AFFDL TR 72-42 Volume 1
Author(s): Batt, James R.; Jordan, Stephen
Corporate Author: Bell Aerospace Co Buffalo N Y
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 7/1/1972
Pages: 182
Contract: F33615-71-C-1390
Project: 1467
Task: 146702
AD Number: AD0755368
Photo Enhancement: Not Needed
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MAGIC III: An Automated General Purpose System for Structural Analysis. Volume II. User's Manual.
Report Number: AFFDL TR 72-42 Volume 2
Author(s): Jordan, Stephen; Batt, James R.
Corporate Author: Bell Aerospace Co Buffalo N Y
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 7/1/1972
Pages: 452
Contract: F33615-71-C-1390
Project: 1467
Task: 146702
AD Number: AD0755369
Photo Enhancement: Not Needed
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MAGIC III: An Automated General Purpose System for Structural Analysis. Volume III. Programmer's Manual.
Report Number: AFFDL TR 72-42 Volume 3
Author(s): Gallo,A. Michael
Corporate Author: Bell Aerospace Co Buffalo N Y
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 7/1/1972
Pages: 728
Contract: F33615-71-C-1390
Project: 1467
Task: 146702
AD Number: AD0755370
Photo Enhancement: Not Needed
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A Study of the Effects of Parameter Variation on the Flying Qualities of the XV-4B V/STOL Aircraft
Report Number: AFFDL TR 72-44
Author(s): Arthur G. Jones
Corporate Author: Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 3/1/1972
Pages: 138
Contract: Laboratory Research - No Contract
Project: 8219
Task: 821907
AD Number: AD0744104
Photo Enhancement: Not Needed
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Atmospheric Turbulence Field Parameters Determination
Report Number: AFFDL TR 72-51
Author(s): Robert L. Neulieb; Jan N. Garrison; Dennis J. Golden
Corporate Author: Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 4/1/1972
Pages: 52
Contract: Laboratory Research - No Contract
Project: 1367
Task: 136702
AD Number: AD0745946
Photo Enhancement: Not Needed
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Experimental and Analytical Investigation of Temperature Sensitive Paints.
Report Number: AFFDL TR 72-52
Author(s): Schultz, Howard D.
Corporate Author: Lockheed Missiles And Space Co Inc Sunnyvale, Calif
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 6/1/1972
Pages: 108
Contract: F33615-71-C-1635
Project: 1366
Task: 136607
AD Number: AD0749582
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Finite Element Modeling and Optimization of Aerospace Structures
Report Number: AFFDL TR 72-59
Author(s): Dwyer, Walter J.
Corporate Author: Grumman Aerospace Corp Bethpage N Y
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 8/1/1972
Pages: 58
Contract: F33615-71-C-1466
Project: 1467
Task: 146701
AD Number: AD0754915
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The Design of Stability Augmentation Systems for Decoupling Aircraft Responses
Report Number: AFFDL TR 72-63
Author(s): Rhall E. Pope
Corporate Author: Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 6/1/1972
Pages: 152
Contract: Laboratory Research - No Contract
Project: 8219
Task: 821904
AD Number: AD0747017
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Abstract Text:
Tactical aircraft with STOL capability exhibit undesirable coupled response during the landing phase of flight. A simplified method for designing a stability augmentation system which eliminates the coupling effects is demonstrated. The method is based on Gilbert's decoupling theory which utilizes a feedback control law to obtain a set of single input, single output subsystems. The augmentation system can be designed to provide either command rate or command angle authority in the three rotational axes. Analyses is facilitated through the use of two computer programs, the first of which determines the class of control laws which will decouple a system. The second computer program determines, through transient response analysis, the values of the transfer function parameters required to satisfy response criteria. The results of a piloted simulation which analyzed several decoupled configurations is also presented.
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Development of an Understanding of the Fatigue Phenomena of Bonded and Bolted Joints in Advanced Filamentary Composite Materials. Volume I. Analysis Methods.
Report Number: AFFDL TR 72-64 Volume 1
Author(s): Dickson, John N.; Hsu,Teh-Min; McKinney,James M.
Corporate Author: Lockheed-Georgia Co Marietta
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 6/1/1972
Pages: 136
Contract: F33615-70-C-1302
Project: None Given
Task: None Given
AD Number: AD0750132
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Development of an Understanding of the Fatigue Phenomena of Bonded and Bolted Joints in Advanced Filamentary Composite Materials. Volume II. Fabrication, Inspection and Testing.
Report Number: AFFDL TR 72-64 Volume 2
Author(s): Fehrle, Albert C.; Gilbert, Gerald J.; Young,Edward C.
Corporate Author: Lockheed-Georgia Co Marietta
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 6/1/1972
Pages: 328
Contract: F33615-70-C-1302
Project: 4364
Task: None Given
AD Number: AD0750133
Photo Enhancement: Complete
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Development of an Understanding of the Fatigue Phenomena of Bonded and Bolted Joints in Advanced Filamentary Composite Materials. Volume 3. Fatigue Analysis and Fatigue Mode Studies.
Report Number: AFFDL TR 72-64 Volume 3
Author(s): Fehrle, A. C. Carroll, J. R. Freeman, S. M.
Corporate Author: Lockheed-Georgia Co Marietta
Publication Date: 6/1/1972
Features: + Foldout(s)
Project: 0
Task: 0
AD Number: ADA308092
Photo Enhancement: Incomplete
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Interference Heating Due to Shock Impingement
Report Number: AFFDL TR 72-66
Author(s): Haslett, Robert A.; Haufman, Louis G. , II.; Romanowski, Richard F.; Urkowitz,Michael
Corporate Author: Grumman Aerospace Corp Bethpage N Y
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 7/1/1972
Pages: 178
Contract: F33615-71-C-1383
Project: 1366
Task: None Given
AD Number: AD0749946
Photo Enhancement: Complete
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Computational Algorithms for Unconstrained Optimization
Report Number: AFFDL TR 72-77
Author(s): Kujawski, Bruce T.
Corporate Author: Air Force Flight Dynamics Lab Wright-Patterson AFB Ohio
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 10/1/1972
Pages: 60
Contract: Laboratory Research - No Contract
Project: 8219
Task: 821911
AD Number: AD0753416
Photo Enhancement: Not Needed
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Evaluation of Advanced Beryllium Structural Configurations.
Report Number: AFFDL TR 72-95
Author(s): Dutko, Theodore R.; Brunken, Ronald D.; Moore, Roy G.
Corporate Author: North American Rockwell Corp Los Angeles CA Los Angeles Div
Publication Date: 9/1/1972
Features: + Foldout(s)
Project: 0
Task: 0
AD Number: AD0904811
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Development of Theoretical Method for Two-Dimensional Multi-Element Airfoil Analysis and Design. Part I: Viscous-Flow Analysis Method.
Report Number: AFFDL TR 72-96 Part 1
Author(s): Bhateley, Ishwar C.; McWhirter, Jack W.
Corporate Author: General Dynamics Fort Worth Tex Convair Aerospace Div
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 8/1/1972
Pages: 380
Contract: F33615-71-C-1597
Project: 1366
Task: None Given
AD Number: AD0749484
Photo Enhancement: Not Needed
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Development of Theoretical Method for Two-Dimensional Multi-Element Airfoil Analysis and Design. Part II: Leading-Edge Slat Design Method.
Report Number: AFFDL TR 72-96 Part 2
Author(s): McGregor, O. Wayne; McWhirter, Jack W.
Corporate Author: General Dynamics Fort Worth Tex Convair Aerospace Div
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 8/1/1972
Pages: 176
Contract: F33615-71-C-1597
Project: 1366
Task: None Given
AD Number: AD0749485
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Notes: Original and pdf missing pages 81-87
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Examination of the Voice Command Concept for Application to Air Force Cockpits
Report Number: AFFDL TR 72-108
Author(s): John M. Reising
Corporate Author: Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 2/5/1973
Pages: 58
Contract: Laboratory Research - No Contract
Project: 6190
Task: None Given
AD Number: AD0762922
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Human Engineering for the Air Force Control-Display Program
Report Number: AFFDL TR 72-109
Author(s): Snyder,Thomas A.; McTee, A. C.
Corporate Author: Bunker-Ramo Corp Westlake Village Calif Electronic Systems Div
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 6/1/1972
Pages: 60
Contract: F33615-69-C-1716
Project: 6190
Task: 619007
AD Number: AD0754916
Photo Enhancement: Not Needed
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VFR Approach Profiles in the T-38 Aircraft
Report Number: AFFDL TR 72-110
Author(s): A. C. McTee
Corporate Author: Bunker Ramo Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 6/1/1972
Pages: 42
Contract: F33615-69-C-1716
Project: 6190
Task: None Given
AD Number: AD0765199
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Multiwheel Landing Gear/Soil Interaction - Phase III. Braked Wheel Sinkage Prediction Technique and Computer Program.
Report Number: AFFDL TR 72-111
Author(s): Bogner, Fred K
Corporate Author: Dayton Univ Oh Research Inst
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 9/1/1972
Pages: 82
Contract: F33615-70-C-1170
Project: 1369
Task: 136908
AD Number: AD0907002
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Application of Cold Plates to Electronic Equipment Cooling
Report Number: AFFDL TR 72-128
Author(s): Feldmanis, Carl J.
Corporate Author: Air Force Flight Dynamics Lab Wright-Patterson AFB OH
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 11/1/1972
Pages: 124
Contract: Laboratory Research - No Contract
Project: 6146
Task: None Given
AD Number: AD0906907
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In-Flight Simulation of Minimum Longitudinal Stability for Large Delta-Wing Transports in Landing Approach and Touchdown: Volume I: Technical Results
Report Number: AFFDL TR 72-143 Volume 1
Author(s): Richard Wasserman; John F. Mitchell
Corporate Author: Calspan Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 2/1/1973
Pages: 134
Contract: F33615-72-C-1386
Project: 920K
Task: None Given
AD Number: AD0761120
Photo Enhancement: Complete
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In-Flight Simulation of Minimum Longitudinal Stability for Large Delta-Wing Transports in Landing Approach and Touchdown: Volume II: Supporting Technical Data and Analysis
Report Number: AFFDL TR 72-143 Volume 2
Author(s): Richard Wasserman; John F. Mitchell; William W. Rickard; Ronald W. Huber; Arno E. Schelhorn
Corporate Author: Calspan Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 2/1/1973
Pages: 258
Contract: F33615-72-C-1386
Project: 920K
Task: None Given
AD Number: AD0780098
Photo Enhancement: Not Needed
Notes: Not from original; likely from microfiche
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