Author: "Lean F" / Publisher: nasa center for aerospace information (casi) - Searchworks@Jio Institute Digital Library Search Results

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Your search keyword '"Lean F"' showing total 11 results

Start Over Author "Lean F" Publisher nasa center for aerospace information (casi)

11 results on '"Lean F"'

1. Sonic-boom characteristics of proposed supersonic and hypersonic airplanes

Author: Carlson, H. W, Hunton, L. W, and Mc Lean, F. E
Subjects: Aircraft
Abstract: Sonic boom characteristics of proposed supersonic and hypersonic aircraft
Published: 1966

2. Effects of thickness on supersonic performance of a wing-body configuration employing a warped highly swept arrow wing

Author: Fuller, D. E and Mc Lean, F. E
Subjects: Aerodynamics
Abstract: Effects of airfoil section shape and thickness on supersonic performance characteristics of wing body configuration employing warped highly swept arrow wing
Published: 1965

3. Aerodynamic characteristics in pitch of several m-wing-body combinations at mach numbers of 2.40, 2.60, and 2.86

Author: Mc Lean, F. E and Morris, O. A
Subjects: Aerodynamics
Abstract: Longitudinal stability and control characteristic of M wing aircraft at various Mach numbers
Published: 1965

4. Some nonasymptotic effects on the sonic boom of large airplanes

Author: Mc Lean, F. E
Subjects: Aircraft
Abstract: Nonasymptotic effects on sonic boom of supersonic transport aircraft
Published: 1965

5. Prediction of airplane sonic-boom pressure fields

Author: Carlson, H. W, Mc Lean, F. E, and Middleton, W. D
Subjects: Aircraft
Abstract: Sensitivity of supersonic-transport design and operation to sonic boom
Published: 1965

6. Design Methods for Minimization of Sonic-boom Pressure-field Disturbances

Author: Mc Lean, F. E and Shrout, B. L
Subjects: Aircraft
Abstract: Design methods for minimizing sonic boom pressure field disturbances
Published: 1965

7. MEASUREMENTS OF FLOW ANGLES IN VICINITY OF TWO LIFTING FOREBODY CONFIGURATIONS AT A MACH NUMBER OF 2.01

Author: Mc Lean, F. E and Morris, O. A
Subjects: Auxiliary Systems
Abstract: Flow angles in vicinity of lifting forebodies at mach 2.01
Published: 1963

8. Supersonic aerodynamic characteristics of some simplified and complex aircraft configurations which employ highly swept twisted-and-cambered arrow-wing planforms

Author: Fuller, D. E and Mc Lean, F. E
Subjects: Biosciences
Abstract: Aerodynamic characteristics of aircraft configurations with highly swept twisted and cambered arrow wings at hypersonic speeds
Published: 1963

9. SUPERSONIC AERODYNAMIC CHARACTERISTICS OF SOME SIMPLIFIED AND COMPLEX AIRCRAFT CONFIGURATIONS WHICH EMPLOY HIGHLY SWEPT TWISTED-AND-CAMBERED ARROW-WING PLANFORMS

Author: Fuller, D. E and Mc Lean, F. E
Subjects: Biosciences
Abstract: Application of low drag-due-to-lift concept of linearized theory to the studies of twist and camber of isolated wing and wing-body configurations of supersonic aircraft
Published: 1963

10. THEORETICAL AND EXPERIMENTAL STUDIES OF CAMBERED AND TWISTED WINGS OPTIMIZED FOR FLIGHT AT SUPERSONIC SPEEDS

Author: Brown, C. E, Klunker, E. B, and Mc Lean, F. E
Subjects: Auxiliary Systems
Abstract: Wing and wing-body design of supersonic aircraft for high aerodynamic efficiency
Published: 1962

11. Theoretical and Experimental Studies of Cambered and Twisted Wings Optimized for Flight at Supersonic Speeds

Author: Brown, C. E, Klunker, E. B, and Mc Lean, F. E
Subjects: Aircraft Design, Testing And Performance, Aerodynamics, Aeronautics (General)
Published: 1960

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