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Direct Side Force Control (DSFC) for STOL Crosswind Landings
Report Number: AFFDL TR 73-2
Author(s): Edward M. Boothe; Howard J. Ledder
Corporate Author: Calspan Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 2/1/1973
Pages: 262
Contract: F33615-72-C-1712
Project: 643A
Task: None Given
AD Number: AD0759555
Photo Enhancement: Complete
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STOL Tactical Aircraft Investigation Volume I Configuration Definition: Medium STOL Transport with Vectored Thrust/Mechanical Flaps
Report Number: AFFDL TR 73-19 Volume 1
Author(s): Richard H. Carroll; John W. Jants; Peter Milns
Corporate Author: The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratoryv
Publication Date: 5/1/1973
Pages: 180
Features: + Foldout(s)
Contract: F33615-71-C-1757
Project: 643A
Task: None Given
AD Number: AD0766637
Photo Enhancement: Not Needed
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STOL Tactical Aircraft Investigation Volume II, Part I Aerodynamic Technology: Design Compendium, Vectored Thrust/Mechanical Flaps
Report Number: AFFDL TR 73-19 Volume 2 Part 1
Author(s): William J. Runciman; Gary R. Letsinger; Bernard F. Ray; Fred W. May
Corporate Author: The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratoryv
Publication Date: 5/1/1973
Pages: 240
Contract: F33615-71-C-1757
Project: 643A
Task: None Given
AD Number: AD0766639
Photo Enhancement: Not Needed
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STOL Tactical Aircraft Investigation Volume II, Part II A Lifting Line Analysis Method for Jet-Flapped Wings
Report Number: AFFDL TR 73-19 Volume 2 Part 2
Author(s): Franklyn J. Davenport
Corporate Author: The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratoryv
Publication Date: 6/1/1973
Pages: 118
Contract: F33615-71-C-1757
Project: 643A
Task: None Given
AD Number: AD0766877
Photo Enhancement: Not Needed
Notes: Some pages blank; printing error
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STOL Tactical Aircraft Investigation Volume III Takeoff and Landing Performance Ground Rules for Powered Lift STOL Transport Aircraft
Report Number: AFFDL TR 73-19 Volume 3
Author(s): Franklyn J. Davenport; Arnold E. Rengstorff; Vernon F. Van Heyningen
Corporate Author: The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratoryv
Publication Date: 5/1/1973
Pages: 59
Features: + Foldout(s)
Contract: F33615-71-C-1757
Project: 643A
Task: None Given
AD Number: AD0766640
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STOL Tactical Aircraft Investigation Volume IV Analysis of Wind Tunnel Data: Vectored Thrust/Mechanical Flaps and Internally Blown Jet Flaps
Report Number: AFFDL TR 73-19 Volume 4
Author(s): John R. Monk; Jerry E. Lee; J. Patrick Palmer
Corporate Author: The Boeing Company
Corp. Rep. Number: D180-14411-1
Laboratory: Air Force Flight Dynamics Laboratoryv
Publication Date: 5/1/1973
Pages: 300
Features: + Diagram(s) + Drawing(s) + Foldout(s) + Graph(s) + Photo(s) + Table(s)
Contract: F33615-71-C-1757
Project: 643A
Task: None Given
AD Number: AD0766641
Photo Enhancement: Complete
Abstract Text:
The report presents the analysis of 728 hours of testing, conducted in the Boeing V/STOL 20 x 20 ft. Wind Tunnel, on a model of a medium STOL transport with vectored thrust and jet flap powered-lift systems. The interactions between the two powered lift systems and the basic airplane aerodynamics are presented for a systematic series of configuration changes which include sweep and nacelle location.
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STOL Tactical Aircraft Investigation Volume V, Part I Flight Control Technology: System Analysis and Trade Studies for a Medium STOL Transport with Vectored Thrust/Mechanical Flaps
Report Number: AFFDL TR 73-19 Volume 5 Part 1
Author(s): Kenneth J. Crandall; David J. Maund; William E. Gerken; James H. Vincent
Corporate Author: The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratoryv
Publication Date: 5/1/1973
Pages: 257
Features: + Foldout(s)
Contract: F33615-71-C-1757
Project: 643A
Task: None Given
AD Number: AD0766642
Photo Enhancement: Not Needed
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STOL Tactical Aircraft Investigation Volume VI Air Cushion Landing System Study
Report Number: AFFDL TR 73-19 Volume 6
Author(s): Lloyd H. Gardner; Charles J. Pizzichemi; Peter Milns
Corporate Author: The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratoryv
Publication Date: 5/1/1973
Pages: 107
Features: + Foldout(s)
Contract: F33615-71-C-1757
Project: 643A
Task: None Given
AD Number: AD0766644
Photo Enhancement: Not Needed
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STOL Tactical Aircraft Investigation - Externally Blown Flap Volume I Configuration Definition
Report Number: AFFDL TR 73-20 Volume 1
Author(s): H. G. Owens; D. J. Renselaer; R. S. Kaneshiro; D. W. Schlundt, et al
Corporate Author: Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratoryv
Publication Date: 4/1/1973
Pages: 370
Features: + Foldout(s)
Contract: F33615-71-C-1760
Project: 643A
Task: None Given
AD Number: AD0772738
Photo Enhancement: Not Needed
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STOL Tactical Aircraft Investigation - Externally Blown Flap Volume I Configuration Definition Supplement I Aerodynamic Trades of Flap and Roll Control System
Report Number: AFFDL TR 73-20 Volume 1 Supplement 1
Author(s): D. J. Renselaer
Corporate Author: Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratoryv
Publication Date: 4/1/1973
Pages: 126
Contract: F33615-71-C-1760
Project: 643A
Task: None Given
AD Number: AD0767179
Photo Enhancement: Not Needed
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STOL Tactical Aircraft Investigation - Externally Blown Flap Volume II Design Compendium
Report Number: AFFDL TR 73-20 Volume 2
Author(s): M. H. Roe; D. J. Renselaer; R. A. Quam et al
Corporate Author: Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratoryv
Publication Date: 4/1/1973
Pages: 184
Contract: F33615-71-C-1760
Project: 643A
Task: None Given
AD Number: AD0770110
Photo Enhancement: Not Needed
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STOL Tactical Aircraft Investigation - Externally Blown Flap Volume III Performance Methods and Takeoff and Landing Rules
Report Number: AFFDL TR 73-20 Volume 3
Author(s): D. J. Renselaer
Corporate Author: Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratoryv
Publication Date: 4/1/1973
Pages: 162
Contract: F33615-71-C-1760
Project: 643A
Task: None Given
AD Number: AD0767180
Photo Enhancement: Not Needed
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STOL Tactical Aircraft Investigation - Externally Blown Flap Volume IV Analysis of Wind Tunnel Data
Report Number: AFFDL TR 73-20 Volume 4
Author(s): P. P. Papp; R. A. Quam; G. A. Freeman
Corporate Author: Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratoryv
Publication Date: 4/1/1973
Pages: 420
Features: + Foldout(s)
Contract: F33615-71-C-1760
Project: 643A
Task: None Given
AD Number: AD0772774
Photo Enhancement: Incomplete
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STOL Tactical Aircraft Investigation - Externally Blown Flap Volume V Flight Control Technology Part I. Control System Mechanization Trade Studies
Report Number: AFFDL TR 73-20 Volume 5 Part 1
Author(s): R. W. Phillips
Corporate Author: Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratoryv
Publication Date: 4/1/1973
Pages: 68
Contract: F33615-71-C-1760
Project: 643A
Task: None Given
AD Number: AD0767181
Photo Enhancement: Not Needed
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STOL Tactical Aircraft Investigation - Externally Blown Flap Volume V Flight Control Technology Part II Simulation Studies/Flight Control System Validation
Report Number: AFFDL TR 73-20 Volume 5 Part 2
Author(s): J. E. Campbell; W. K. Elsanker; V. H. Okomuto
Corporate Author: Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratoryv
Publication Date: 4/1/1973
Pages: 214
Contract: F33615-71-C-1760
Project: 643A
Task: None Given
AD Number: AD0770449
Photo Enhancement: Complete
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STOL Tactical Aircraft Investigation - Externally Blown Flap Volume V Flight Control Technology Part III Stability and Control Derivative Accuracy Requirements and Effects of Augmentation System Design
Report Number: AFFDL TR 73-20 Volume 5 Part 3
Author(s): W. K. Elsanker; V. H. Okomoto
Corporate Author: Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 4/1/1973
Pages: 202
Contract: F33615-71-C-1760
Project: 643A
Task: None Given
AD Number: AD0767182
Photo Enhancement: Not Needed
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STOL Tactical Aircraft Investigation - Externally Blown Flap: Volume VI Air Cushion Landing System Trade Study
Report Number: AFFDL TR 73-20 Volume 6
Author(s): R. G. Gustavson
Corporate Author: Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 4/1/1973
Pages: 87
Features: + Foldout(s)
Contract: F33615-71-C-1760
Project: 643A
Task: None Given
AD Number: AD0770448
Photo Enhancement: Not Needed
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STOL Tactical Aircraft Investigation: Volume I Configuration Definition
Report Number: AFFDL TR 73-21 Volume 1
Author(s): J. Herbert, et al
Corporate Author: General Dynamics Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 5/1/1973
Pages: 169
Features: + Foldout(s)
Contract: F33615-71-C-1754
Project: 643A
Task: None Given
AD Number: AD0766941
Photo Enhancement: Not Needed
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STOL Tactical Aircraft Investigation: Volume II Design Compendium
Report Number: AFFDL TR 73-21 Volume 2
Author(s): J. Herbert, Jr.; E. S. Levinsky; J. C. Ramsey; E. C. Laudeman; H. G. Altman; L. G. Barbee
Corporate Author: General Dynamics Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 5/1/1973
Pages: 272
Features: + Foldout(s)
Contract: F33615-71-C-1754
Project: 643A
Task: None Given
AD Number: AD0767561
Photo Enhancement: Not Needed
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STOL Tactical Aircraft Investigation: Volume III Performance Ground Rules and Methods Book 2 Takeoff and Landing Ground Rules
Report Number: AFFDL TR 73-21 Volume 3 Book 1
Author(s): J. Herbert, Jr.; C. A. Whitney; E. C. Laudeman; G. T. Draper
Corporate Author: General Dynamics Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 5/1/1973
Pages: 56
Contract: F33615-71-C-1754
Project: 643A
Task: None Given
AD Number: AD0766942
Photo Enhancement: Not Needed
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STOL Tactical Aircraft Investigation: Volume III Performance Ground Rules and Methods Book 2 Takeoff and Landing Digital Computer Program
Report Number: AFFDL TR 73-21 Volume 3 Book 2
Author(s): J. Herbert, Jr.; C. A. Whitney
Corporate Author: General Dynamics Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 5/1/1973
Pages: 138
Contract: F33615-71-C-1754
Project: 643A
Task: None Given
AD Number: AD0766943
Photo Enhancement: Not Needed
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STOL Tactical Aircraft Investigation: Volume IV Wind Tunnel Data Analysis
Report Number: AFFDL TR 73-21 Volume 4
Author(s): J. Herbert, Jr.; J. C. Ramsey; E. C. Laudeman; N. A. Ponomareff; H. Altman
Corporate Author: General Dynamics Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 5/1/1973
Pages: 410
Contract: F33615-71-C-1754
Project: 643A
Task: None Given
AD Number: AD0767363
Photo Enhancement: Complete
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STOL Tactical Aircraft Investigation: Volume V Flight Control Technology
Report Number: AFFDL TR 73-21 Volume 5
Author(s): J. Herbert, Jr.; G. Campbell; E. Price; L. B. White; R. Halstenberg
Corporate Author: General Dynamics Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 5/1/1973
Pages: 356
Contract: F33615-71-C-1754
Project: 643A
Task: None Given
AD Number: AD0767364
Photo Enhancement: Complete
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STOL Tactical Aircraft Investigation: Volume VI Air Cushion and Ground Mobility Study
Report Number: AFFDL TR 73-21 Volume 6
Author(s): J. Herbert, Jr.; H. Weber; G. T. Draper; C. Kerr, Jr.; T. F. Reid
Corporate Author: General Dynamics Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 5/1/1973
Pages: 44
Contract: F33615-71-C-1754
Project: 643A
Task: None Given
AD Number: AD0767300
Photo Enhancement: Not Needed
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Development and Evaluation of an Automatic Departure Prevention System and Stall Inhibitor for Fighter Aircraft
Report Number: AFFDL TR 73-29
Author(s): Robert T. N. Chen; Fred D. Newell; Arno E. Schelhorn
Corporate Author: Calspan Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 4/1/1973
Pages: 124
Features: + Foldout(s)
Contract: F33615-72-C-1162
Project: 8225
AD Number: AD0764767
Photo Enhancement: Complete
Abstract Text:
The report documents the conceptual design, breadboard development and pilot-in-the-loop evaluation of an automatic departure prevention system and a stall inhibitor for fighter aircraft. Using the A-7D as the study aircraft, a departure boundary characterized by alpha and beta was determined from the available data. This departure boundary was then used to help design an automatic departure preventer and a stall inhibitor. An automatic departure prevention device as described in the report works smoothly and will benefit the A-7 aircraft. With just the departure preventer, the pilots could maneuver freely, with great confidence and use the full capability of the airplane, well beyond the present departure boundary.
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Flight Simulator Experiments and Analyses in Support of Further Development of MIL-F-83300 - V/STOL Flying Qualities Specification
Report Number: AFFDL TR 73-34
Author(s): Edward W. Vinje; David P. Miller
Corporate Author: United Aircraft Research Laboratories
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 6/1/1973
Pages: 248
Contract: F33615-71-C-1722
Project: 643A
Task: None Given
AD Number: AD0769868
Photo Enhancement: Complete
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Design, Development, and Flight Test of Multiplexing Hardware for Use in a Fly-by-Wire Flight Control System
Report Number: AFFDL TR 73-43
Author(s): J. G. Mrazek; R. O. Roberts
Corporate Author: General Dynamics
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 4/1/1973
Pages: 108
Features: + Foldout(s)
Contract: F33615-71-C-1147
Project: 8225
Task: None Given
AD Number: AD0763111
Photo Enhancement: Complete
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An Analytical and Experimental Investigation of Hypersonic Viscous Interaction Pressure Effects
Report Number: AFFDL TR 73-58
Author(s): Neil J. Sliski
Corporate Author: Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 11/1/1973
Pages: 102
Contract: Laboratory Research - No Contract
Project: 1366
Task: 136607
AD Number: AD0778487
Photo Enhancement: Not Needed
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Recommended Revisions to Selected Portions of MIL-F-8785B (ASG) and Background Data
Report Number: AFFDL TR 73-76
Author(s): Irving L. Ashkenas; Roger H. Hoh; Samuel J. Craig
Corporate Author: Systems Technology, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 8/1/1973
Pages: 176
Contract: F33615-72-C-1456
Project: None Given
Task: None Given
AD Number: ADA002633
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Structural Mode Effects on Flying Qualities in Turbulence
Report Number: AFFDL TR 73-88
Author(s): C. A. Crother; B. Gabelman; D. Langton
Corporate Author: Los Angeles Aircraft
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 8/1/1973
Pages: 418
Contract: F33615-71-C-1418
Project: 8219
Task: 821904
AD Number: ADA004416
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Fighter Technology Demonstrator Precursor Analysis and Test: Volume I. Baseline Development and Technology Identification
Report Number: AFFDL TR 73-112 Volume 1
Author(s): None Given
Corporate Author: Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 11/1/1973
Pages: 270
Features: + Foldout(s)
Contract: F33615-73-C-3135
Project: 1207
Task: None Given
AD Number: AD0783636
Photo Enhancement: Incomplete
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Fighter Technology Demonstrator Precursor Analysis and Test: Volume II - An Experimental Investigation of the Aerodynamic Characteristics of a Fighter Technology Demonstrator Jet Flap Development Model at Low Subsonic Mach Number
Report Number: AFFDL TR 73-112 Volume 2
Author(s): G. N. Panageas
Corporate Author: Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 11/1/1973
Pages: 112
Contract: F33615-73-C-3135
Project: 1207
Task: None Given
AD Number: AD0779742
Photo Enhancement: Complete
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Identification and Correlation of the F-4E Stall/Post-Stall Aerodynamic Stability and Control Characteristics from Existing Test Data
Report Number: AFFDL TR 73-125
Author(s): Bernard J. Eulrich; Norman C. Weingarten
Corporate Author: Calspan Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 11/1/1973
Pages: 334
Contract: F33615-72-C-1248
Project: 8219
Task: 821902
AD Number: AD0779928
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Abstract Text:
The report documents the results of a study performed for the United States Air Force Flight Dynamics Laboratory to identify the high angle of attack post stall aerodynamic stability and control characteristics of the F-4 aircraft from existing full scale and radio-controlled drop model test data and to correlate these results with similar characteristics obtained from wind tunnel tests. A parameter identification procedure was set up to extract these nonlinear characteristics from flight test records using a nonlinear iterated Kalman filter/fixed-point smoother algorithm and a least square equation error method. Model form is established from wind tunnel data by representing the aerodynamic coefficients by Taylor's series expansions for selected ranges of angle of attack.
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Design Methods for Specifying Handling Qualities for Control Configured Vehicles: Volume II Mcpilot Program User's Manual
Report Number: AFFDL TR 73-142 Volume 2
Author(s): D. W. Vogt
Corporate Author: McDonnell Aircraft Company
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 11/1/1973
Pages: 252
Contract: F33615-73-C-3064
Project: 8219
Task: 821903
AD Number: AD0779731
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Methods for Predicting the Aerodynamic and Stability and Control Characteristics of STOL Aircraft. Volume I. Basic Theoretical Methods.
Report Number: AFFDL TR 73-146 Volume 1
Author(s): M. I. Goldhammer; M. L. Lopez; C. C. Shen
Corporate Author: Douglas Aircraft Company
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1973
Pages: 275
Contract: F33615-71-C-1861
Project: 643A
AD Number: ADA001580
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Abstract Text:
The primary goal of the study has been the development of a unified set of analytical methods which would provide the capability to calculate the stability and control characteristics of an arbitrary STOL aircraft configuration that might employ the internally ducted jet flap, externally blown jet flap, or a mechanical high lift system with vectored thrust. This volume presents the complete theoretical development of the relevant analytical methods. In addition, it presents comparisons of these methods with other analytical solutions and with experimental data.
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Methods for Predicting the Aerodynamic and Stability and Control Characteristics of STOL Aircraft: Volume II STOL Aerodynamic Methods Computer Program
Report Number: AFFDL TR 73-146 Volume 2
Author(s): M. I. Goldhammer; N. F. Wasson
Corporate Author: Douglas Aircraft Company
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1973
Pages: 230
Contract: F33615-71-C-1861
Project: 643A
Task: None Given
AD Number: ADA001581
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Methods for Predicting the Aerodynamic and Stability and Control Characteristics of STOL Aircraft: Volume III Engineering Methods
Report Number: AFFDL TR 73-146 Volume 3
Author(s): M. I. Goldhammer; M. L. Lopez
Corporate Author: Douglas Aircraft Company
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1973
Pages: 256
Contract: F33615-71-C-1861
Project: 643A
Task: None Given
AD Number: ADA001582
Photo Enhancement: Not Needed
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The Effect of Ground Proximity on the Lateral/Directional Aerodynamic and Control Characteristics of a Tilt-Wing V/STOL Aircraft at High Lift Coefficients
Report Number: AFFDL TR 73-151
Author(s): H. C. Curtiss, Jr.; J. J. Traybar; W. F. Putnam
Corporate Author: Princeton University
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1973
Pages: 164
Contract: F33615-71-C-1206
Project: 8219
Task: None Given
AD Number: ADA001584
Photo Enhancement: Complete
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Acoustic Fatigue of Aircraft Structures at Elevated Temperatures
Report Number: AFFDL TR 73-155 Part 1
Author(s): Cecil W. Schneider
Corporate Author: Lockheed-Georgia Company
Corp. Rep. Number: LG73ER0182
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 3/1/1974
Pages: 219
Contract: F33615-72-C-1141
Project: 1471
Task: 147101
AD Number: AD0920282
Abstract Text:
An analytical and experimental program was conducted to develop acoustic fatigue design criteria for aircraft structures subjected to intense noise in a high temperature environment. Equations for the dynamic response of a buckled panel were formulated for simply supported boundary conditions using large deflection plate theory. Random amplitude acoustic fatigue testing of representative aircraft structure was accomplished at temperatures up to 600 F to provide data for correlation with the analytical results. Empirical design criteria are presented in the form of design equations and nomographs for predicting the combined thermal and dynamic response of aircraft structures.
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Acoustic Fatigue of Aircraft Structures at Elevated Temperatures
Report Number: AFFDL TR 73-155 Part 2
Author(s): Cecil W. Schneider
Corporate Author: Lockheed-Georgia Company
Corp. Rep. Number: LG73ER0183
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 3/1/1974
Pages: 77
Contract: F33615-72-C-1141
Project: 1471
Task: 147101
AD Number: AD0920427
Abstract Text:
An analytical and experimental program was conducted to develop acoustic fatigue design criteria for aircraft structures subjected to intense noise in a high temperature environment. Equations for the dynamic response of a buckled panel were formulated for simply supported boundary conditions using large deflection plate theory. Random amplitude acoustic fatigue testing of representative aircraft structure was accomplished at temperatures up to 600 deg F to provide data for correlation with the analytical results. Empirical design criteria were developed in the form of equations and nomographs for predicting the thermal and dynamic response of aircraft structures subjected to combined environments. The empirical design criteria are presented in handbook format for design use; examples and computer programs are also presented.
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The Mark IV Supersonic-Hypersonic Arbitrary-Body Program. Volume I. User's Manual
Report Number: AFFDL TR 73-159 Volume 1
Author(s): Arvel E. Gentry; Douglas N. Smith; Wayne R. Oliver
Corporate Author: McDonnell Douglas Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 11/1/1973
Pages: 268
Project: 0
Task: 0
AD Number: AD0778443
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The Mark IV Supersonic-Hypersonic Arbitrary-Body Program. Volume II. Program Formulation
Report Number: AFFDL TR 73-159 Volume 2
Author(s): Arvel E. Gentry; Douglas N. Smyth; Wayne R. Oliver
Corporate Author: McDonnell Douglas Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 11/1/1973
Pages: 230
Contract: F33615-72-C-1675
Project: None Given
Task: None Given
AD Number: AD0778444
Photo Enhancement: Not Needed
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The Mark IV Supersonic-Hypersonic Arbitrary Body Program Volume III - Program Listings
Report Number: AFFDL TR 73-159 Volume 3
Author(s): Arvel E. Gentry; Douglas N. Smyth; Wayne R. Oliver
Corporate Author: McDonnell Douglas Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 11/1/1973
Pages: 584
Contract: F33615-72-C-1675
Project: None Given
Task: None Given
AD Number: AD0778445
Photo Enhancement: Not Needed
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