►Airplane Design - Part I - Preliminary Sizing of Airplanes (1985 232p)
►Airplane Design - Part II - Preliminary Configuration Design and Integration of the Propulsion System (1985 322p)
►Airplane Design - Part III -  Layout Design of Cockpit, Fuselage, Wing and Empennage: Cutaways and Inboard Profiles (1986 462p)
►Airplane Design - Part IV -  Layout Design of Landing Gear and Systems (1986 436p)
►Airplane Design - Part V - Component Weight Estimation (1985 227p)
►Airplane Design - Part VI -  Preliminary Calculation of Aerodynamic, Thrust and Power Characteristics (1987 583p)
►Airplane Design - Part VII -  Determination of Stability, Control and Performance Characteristics: FAR and Military Requirements (1986 371p)
►Airplane Design - Part VIII - Airplane Cost Estimation - Design, Development, Manufacturing and Operating (1990 409p)

--- Airplane Design - Part I - Preliminary Sizing of Airplanes
Airplane Design Part I: Preliminary Sizing of Airplanes is the first book in a series of eight volumes on airplane design. The airplane design series has been internationally acclaimed as a practical reference that covers the methodology and decision making involved in the process of designing airplanes. Educators and industry practitioners across the globe rely on this compilation as both a textbook and a key reference. Airplane Design Part I: Preliminary Sizing of Airplanes familiarizes the reader with the following fundamentals: - Estimating take-off gross weight, empty weight and mission fuel weight - Sensitivity studies and growth factors - Estimating wing area - Take-off thrust and maximum clean, take-off and landing lift - Sizing to stall speed, take-off distance, landing distance, climb, maneuvering and cruise speed requirements - Matching of all performance requirements via performance matching diagrams.

--- Airplane Design - Part II - Preliminary Configuration Design and Integration of the Propulsion System
Airplane Design Part II: Preliminary Configuration Design and Integration of the Propulsion System is the second book in a series of eight volumes on airplane design. The airplane design series has been internationally acclaimed as a practical reference that covers the methodology and decision making involved in the process of designing airplanes. Educators and industry practitioners across the globe rely on this compilation as both a textbook and a key reference.

- Selection of the overall configuration
- Design of cockpit and fuselage layouts
- Selection and integration of the propulsion system
- Class I method for wing planform design
- Class I method for verifying clean airplane maximum lift coefficient and for sizing high lift devices
- Class I method for empennage sizing and disposition, control surface sizing and disposition, landing gear sizing and disposition, weight and balance analysis, stability and control analysis and drag polar determination

--- Airplane Design - Part III -  Layout Design of Cockpit, Fuselage, Wing and Empennage: Cutaways and Inboard Profiles
Airplane Design Part III: Layout Design of Cockpit, Fuselage, Wing and Empennage: Cutaways and Inboard Profiles is the third book in a series of eight volumes on airplane design. The airplane design series has been internationally acclaimed as a practical reference that covers the methodology and decision making involved in the process of designing airplanes. Educators and industry practitioners across the globe rely on this compilation as both a textbook and a key reference.

- Cockpit (or flight deck) layout design
- Aerodynamic design considerations for the fuselage layout
- Interior layout design of the fuselage
- Fuselage structural design considerations
- Wing aerodynamic and operational design considerations
- Wing structural design considerations
- Empennage aerodynamic and operational design considerations
- Empennage structural and integration design consideration
- Integration of propulsion system
- Preliminary structural arrangement, material selection and manufacturing breakdown

--- Airplane Design - Part IV -  Layout Design of Landing Gear and Systems
Airplane Design Part IV: Layout Design of Landing Gear and Systems is the fourth book in a series of eight volumes on airplane design. The airplane design series has been internationally acclaimed as a practical reference that covers the methodology and decision making involved in the process of designing airplanes. Educators and industry practitioners across the globe rely on this compilation as both a textbook and a key reference.

- Landing gear layout design
- Weapons integration and weapons data
- Flight control system layout data
- Fuel system layout design
- Hydraulic system design
- Electrical system layout design
- Environmental control system layout design
- Cockpit instrumentation, flight management and avionics system layout design
- De-icing and anti-icing system layout design
- Escape system layout design
- Water and waste systems layout design
- Safety and survivability considerations

--- Airplane Design - Part V - Component Weight Estimation
Airplane Design Part V: Component Weight Estimation is the fifth book in a series of eight volumes on airplane design. The airplane design series has been internationally acclaimed as a practical reference that covers the methodology and decision making involved in the process of designing airplanes. Educators and industry practitioners across the globe rely on this compilation as both a textbook and a key reference. Airplane Design Part V: Component Weight Estimation familiarizes the reader with the following fundamentals: - Class I method for estimating airplane component weights - Class I method for estimating airplane moments of inertia - Class II methods for detailed airplane component and grouping weights - V-n diagram methods - Class II method for structure weight - Class II method for powerplant weight - Class II method for fixed equipment weight - Data and methods for center of gravity location of individual components - Class II method for airplane moments and products of inertia - Data base for airplane component weights - Data base for airplane non-dimensional radii of gyration

--- Airplane Design - Part VI -  Preliminary Calculation of Aerodynamic, Thrust and Power Characteristics
Airplane Design Part VI: Preliminary Calculation of Aerodynamic, Thrust and Power Characteristics is the sixth book in a series of eight volumes on airplane design. The airplane design series has been internationally acclaimed as a practical reference that covers the methodology and decision making involved in the process of designing airplanes. Educators and industry practitioners across the globe rely on this compilation as both a textbook and a key reference. Airplane Design Part VI: Preliminary Calculation of Aerodynamic, Thrust and Power Characteristics, familiarizes the reader with the following fundamentals: - Methods for estimating airplane drag with and without flaps - Methods for estimating airplane lift with and without flaps - Methods for estimating airplane pitching moment with and without flaps - Methods for estimating installed thrust and power data - Methods for estimating stability derivatives - Methods for estimating control derivatives - Methods for estimating hingemoment derivatives.

--- Airplane Design - Part VII -  Determination of Stability, Control and Performance Characteristics: FAR and Military Requirements
Airplane Design Part VII: Determination of Stability, Control and Performance Characteristics is the seventh book in a series of eight volumes on airplane design. The airplane design series has been internationally acclaimed as a practical reference that covers the methodology and decision making involved in the process of designing airplanes. Educators and industry practitioners across the globe rely on this compilation as both a textbook and a key reference.

- Controllability, maneuverability and trim
- Static and dynamic stability
- Ride and comfort characteristics
- Performance prediction methods
- Civil and military airworthiness regulations for airplane performance and stability and control
- The airworthiness code and the relationship between failure states, levels of performance and levels of flying qualities

--- Airplane Design - Part VIII - Airplane Cost Estimation - Design, Development, Manufacturing and Operating
Airplane Design Part VIII: Airplane Cost Estimation: Design, Development, Manufacturing and Operating is the eighth book in a series of eight volumes on airplane design. The airplane design series has been internationally acclaimed as a practical reference that covers the methodology and decision making involved in the process of designing airplanes. Educators and industry practitioners across the globe rely on this compilation as both a textbook and a key reference.

Cost definitions and concepts
Method for estimating research, development, test and evaluation cost
Method for estimating prototyping cost
Method for estimating manufacturing and acquisition cost
Method for estimating operating cost
Example of life cycle cost calculation for a military airplane
Airplane design optimization and design-to-cost considerations
Factors in airplane program decision making