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Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8t̊o 90̊
1. Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8t̊o 90̊

Mulcay, William

Keywords:

    Aerodynamics; Ground Simulators; Spin (Aerodynamics); Wind Tunnels
View @ University of Illinois
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Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8° to 90°
2. Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8° to 90°

Mulcay, William, author Chu, Julio, author

Keywords:

    Aerodynamics; Ground Simulators; Spin (Aerodynamics); Wind Tunnels
View @ United States Government Publishing Office (GPO)
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Utilization of a fixed-base simulator to study the stall and spin characteristics of fighter airplanes
3. Utilization of a fixed-base simulator to study the stall and spin characteristics of fighter airplanes

Keywords:

    Fighter Planes; Spin (Aerodynamics); Stalling (Aerodynamics); Testing
View @ University of Illinois
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A piloted simulation study of operational aspects of the stall pitch-up
4. A piloted simulation study of operational aspects of the stall pitch-up

White, Maurice D

Keywords:

    Flight Simulators; Piloting; Pitching (Aerodynamics); Stalling (Aerodynamics); Transport Planes
View @ University of Illinois
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A study to determine the flight characteristics and handling qualities of variable geometry spacecraft Volume 1, High L/D concept with single pivot two-position skewed wing
5. A study to determine the flight characteristics and handling qualities of variable geometry spacecraft Volume 1, High L/D concept with single pivot two-position skewed wing

Kuchta, B. J

Keywords:

    Aerodynamics; Aerodynamics, Hypersonic; Handling Characteristics; Oblique Wings; Space Vehicles
View @ University of Illinois
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Human transfer characteristics in flight and ground simulation for a roll tracking task
6. Human transfer characteristics in flight and ground simulation for a roll tracking task

Newell, Fred D., author Smith, Harriet J., author

Keywords:

    Aerodynamics; Airplanes; Flight Simulators; Human Factors; Piloting; Rolling (Aerodynamics)
View @ United States Government Publishing Office (GPO)
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Simulator study of the stall departure characteristics of a light general aviation airplane with and without a wing-leading-edge modification
7. Simulator study of the stall departure characteristics of a light general aviation airplane with and without a wing-leading-edge modification

Riley, Donald R

Keywords:

    Airplanes; Leading Edge (Aerodynamics); Stalling (Aerodynamics); Testing; Wings
View @ University of Illinois
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Analysis of a coupled roll-spiral-mode, pilot-induced oscillation experienced with the M2-F2 lifting body
8. Analysis of a coupled roll-spiral-mode, pilot-induced oscillation experienced with the M2-F2 lifting body

Kempel, Robert W

Keywords:

    Aerodynamics; Oscillations
View @ University of Illinois
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Transonic off-design drag and performance of an axisymmetric inlet with 40 percent internal contraction on design
9. Transonic off-design drag and performance of an axisymmetric inlet with 40 percent internal contraction on design

Woollett, Richard R

Keywords:

    Aerodynamic Drag; Aerodynamic Interference; Aerodynamics, Transonic; Air Intakes; Axisymmetric Flow; Drag (Aerodynamics); Engine Inlets; Flow Characteristics; Inlet Flow; Jet Engines; Transonic Flow; Variable Geometry Structures
View @ University of Illinois
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Airborne simulation for the SST
10. Airborne simulation for the SST

Breuhaus, W. O

Keywords:

    Aerodynamics, Supersonic; Flight Simulators
View @ Cornell University
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An approximate determination of the power required to move control surfaces as related to control-booster design
11. An approximate determination of the power required to move control surfaces as related to control-booster design

Johnson, Harold I

Keywords:

    Aerodynamics; Fighter Planes; Research
View @ University of Florida
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Aerodynamic-derivative characteristics of the X-15 research airplane as determined from flight tests for mach numbers from 0.6 to 3.4
12. Aerodynamic-derivative characteristics of the X-15 research airplane as determined from flight tests for mach numbers from 0.6 to 3.4

Yancey, Roxanah B

Keywords:

    Aerodynamics, Aircraft; Aerodynamics, Missiles And Space Vehicles; Aircraft; Piloting; Simulators And Computers; Stability And Control
View @ University of Illinois
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Analysis of a pilot-airplane lateral instability experienced with the X-15 airplane
13. Analysis of a pilot-airplane lateral instability experienced with the X-15 airplane

Taylor, Lawrence W

Keywords:

    Aerodynamics, Aircraft; Aerodynamics, Missiles And Space Vehicles; Aircraft; Simulators And Computers; Stability And Control; Vehicle Performance
View @ University of Illinois
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Effects of gyroscopic cross coupling between pitch and yaw on the handling qualities of VTOL aircraft
14. Effects of gyroscopic cross coupling between pitch and yaw on the handling qualities of VTOL aircraft

Garren, John F

Keywords:

    Gyroscopic Instruments; Handling Characteristics; Pitching (Aerodynamics); Vertically Rising Aircraft; Yawing (Aerodynamics)
View @ University of Illinois
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Real-time aerodynamic heating and surface temperature calculations for hypersonic flight simulation
15. Real-time aerodynamic heating and surface temperature calculations for hypersonic flight simulation

Quinn, Robert D

Keywords:

    Aerodynamic Heating; Aerodynamics, Hypersonic; Computer Programs; Flight Simulators; Real Time Programming
View @ University of Illinois
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A method for simulating the atmospheric entry of long-range ballistic missiles
16. A method for simulating the atmospheric entry of long-range ballistic missiles

Eggers, A. J

Keywords:

    Aerodynamics; Atmospheric Entry; Ballistic Missiles; Research
View @ University of Florida
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Flight investigation of the roll requirements for transport airplanes in the landing approach [electronic resource]
17. Flight investigation of the roll requirements for transport airplanes in the landing approach [electronic resource]

Holleman, Euclid C

Keywords:

    Airplanes; Landing; Rolling (Aerodynamics); Transport Planes
View @ University of Illinois
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Force modification and deflection loss compensation to the pilot's controls in an aircraft simulator
18. Force modification and deflection loss compensation to the pilot's controls in an aircraft simulator

Cleveland, William B

Keywords:

    Aerodynamic Load; Airplanes; Flight Simulators; Piloting
View @ University of Illinois
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Simulator study of the instrument landing approach of a heavy subsonic jet transport with an external-flow jet-flap system used for additional lift
19. Simulator study of the instrument landing approach of a heavy subsonic jet transport with an external-flow jet-flap system used for additional lift

Grantham, William D

Keywords:

    Landing; Lift (Aerodynamics); Takeoff; Transport Planes
View @ University of Illinois
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Analysis of X-15 landing approach and flare characteristics determined from the first 30 flights
20. Analysis of X-15 landing approach and flare characteristics determined from the first 30 flights

Matranga, Gene J

Keywords:

    Aerodynamics, Aircraft; Aerodynamics, Missiles And Space Vehicles; Aircraft; Piloting; Simulators And Computers; Stability And Control; Stresses And Loads; Vehicle Performance
View @ University of Illinois
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