Add to ORKGThe V/STOL Aircraft Propulsive Effects (VAPE) computerized prediction method is evaluated. The program analyzes viscous effects, various jet, inlet, and Short TakeOff and Landing (STOL) models, and examines the aerodynamic configurations of V/STOL aircraft
Instructions for using Vertical Attitude Takeoff and Landing Aircraft Simulation (VATLAS), the digit...
V/STOL short haul transport design considerations including noise characteristic
The linear performance definition curves for the lift fan aircraft, tilt rotor aircraft, and advance...
A computerized prediction method known as the Vought V/STOL Aircraft Propulsive Effects computer pro...
A computer program, VSAERO, has been applied to a number of V/STOL configurations with a view to adv...
A numerical procedure was developed for the aerodynamic force and moment analysis of V/STOL aircraft...
The requirements for satisfactory characteristics in several key technology areas are discussed and ...
The ability of current methodologies to accurately predict the aerodynamic characteristics identifie...
The impact of military applications on rotorcraft and V/STOL aircraft design is summarized with resp...
Basic principles relating to the accomplishment of V/STOL flight are reviewed as they pertain to cur...
An experimental investigation of V/STOL thrust augmenter wings in flight at slow forward speeds is r...
The aerodynamic performance of V/STOL and STOVL fighter/attack aircraft was assessed. Aerodynamic an...
A study has been made of the economic viability of advanced V/STOL aircraft concepts in performing g...
Conceptual designs and analyses were conducted on two V/STOL supersonic fighter/attack aircraft. The...
Vertical short takeoff aircraft capability, supersonic dash capability, and transonic agility were i...
Instructions for using Vertical Attitude Takeoff and Landing Aircraft Simulation (VATLAS), the digit...
V/STOL short haul transport design considerations including noise characteristic
The linear performance definition curves for the lift fan aircraft, tilt rotor aircraft, and advance...
A computerized prediction method known as the Vought V/STOL Aircraft Propulsive Effects computer pro...
A computer program, VSAERO, has been applied to a number of V/STOL configurations with a view to adv...
A numerical procedure was developed for the aerodynamic force and moment analysis of V/STOL aircraft...
The requirements for satisfactory characteristics in several key technology areas are discussed and ...
The ability of current methodologies to accurately predict the aerodynamic characteristics identifie...
The impact of military applications on rotorcraft and V/STOL aircraft design is summarized with resp...
Basic principles relating to the accomplishment of V/STOL flight are reviewed as they pertain to cur...
An experimental investigation of V/STOL thrust augmenter wings in flight at slow forward speeds is r...
The aerodynamic performance of V/STOL and STOVL fighter/attack aircraft was assessed. Aerodynamic an...
A study has been made of the economic viability of advanced V/STOL aircraft concepts in performing g...
Conceptual designs and analyses were conducted on two V/STOL supersonic fighter/attack aircraft. The...
Vertical short takeoff aircraft capability, supersonic dash capability, and transonic agility were i...
Instructions for using Vertical Attitude Takeoff and Landing Aircraft Simulation (VATLAS), the digit...
V/STOL short haul transport design considerations including noise characteristic
The linear performance definition curves for the lift fan aircraft, tilt rotor aircraft, and advance...