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1NASA Technical Reports Server (NTRS) 19650074048: NACA Conference On Aerodynamic Problems Of Transonic Airplane Design Introductory Remarks On Transonic Testing Techniques Preliminary Investigation Of Airfoil Charac- Teristics Near M Equals 1 Wing Characteristics Near And At Maximum Lift For Transonic Speeds Status Of The High-speed Flutter Problem The Rolling Power Of Two Wing-aileron Configu- Rations As Affected By Flexibility The Effect Of Aeroelasticity On The Static Longitudinal Stability Of An Example Swept- Wing Bomber Wing Selection As Influenced By The Effect Of Wing Bending On Aerodynamic-center Shift Loss Of Longitudinal Damping In Pitch Due To Flexibility Of Wings In Bending Drag Characteristics At Zero Lift Of Bodies At Transonic Speeds The Flow Over Moderately Swept Wings At High Subsonic Speeds Including The Effects Of Na- Celle Interference Effect On Force Coefficients Of Bodies Of Rev- Olution Attached To Straight And Swept Wings Assessment Of The Drag Problem Design And Calibration Of Airspeed Installa- Tions Stability Some Effects Of Sweepback And Airfoil Thick- Ness On Longitudinal Stability And Control Characteristics At Transonic Speeds A Comparison Of The Longitudinal Stability And Control Characteristics Of Three Airplane Con- Figurations Downwash And Wake Characteristics At Transonic Speeds Effect Of Stall-control Devices On The Low- Speed Characteristics Of Swept Wings. Part I- Fixed Sweep Effect Of Stall-control Devices On The Low- Speed Characteristics Of Swept Wings. Part Ii- Variable Sweep Effect Of Twist And Camber On The Low-speed Characteristics Of A Swept Wing Preliminary Investigations Of The Effect Of Plan Form Control-surface Characteristics At Transonic Speeds Dynamic Lateral Stability Of Transonic Air- Planes Summary Of Information On Air Inlets- Nose And Wing-root Inlets Diffusers For High-speed Aircraft Analysis Of The Stability Characteristics Of Twin-intake Air-induction Systems Jet Exhaust Characteristics Blade-section Characteristics From Pressure Distributions On The Sections Of Operating Propellers An Experimental Investigation Of Single- Rotation Propeller Characteristics At High- Subsonic Mach Numbers Summary Of Results Of United Aircraft Wind- Tunnel Tests Of A Supersonic Propeller Investigation Of A Dual Propeller At High-Subsonic Mach Numbers Vibration Of Aircraft Propellers Prediction Of First-order Vibratory Stresses For A Propeller Operating In The Flow Field Of A Wing-nacelle-fuselage Combination The Propeller Flutter Problem For High-speed Airplanes Introductory Remarks On Transonic Testing Techniques Preliminary Investigation Of Airfoil Charac- Teristics Near M Equals 1 Wing Characteristics Near And At Maximum Lift For Transonic Speeds Status Of The High-speed Flutter Problem The Rolling Power Of Two Wing-aileron Configu- Rations As Affected By Flexibility The Effect Of Aeroelasticity On The Static Longitudinal Stability Of An Example Swept- Wing Bomber Wing Selection As Influenced By The Effect Of Wing Bending On Aerodynamic-center Shift Loss Of Longitudinal Damping In Pitch Due To Flexibility Of Wings In Bending Drag Characteristics At Zero Lift Of Bodies At Transonic Speeds The Flow Over Moderately Swept Wings At High Subsonic Speeds Including The Effects Of Na- Celle Interference Effect On Force Coefficients Of Bodies Of Rev- Olution Attached To Straight And Swept Wings Assessment Of The Drag Problem Design And Calibration Of Airspeed Installa- Tions Stability Some Effects Of Sweepback And Airfoil Thick- Ness On Longitudinal Stability And Control Characteristics At Transonic Speeds A Comparison Of The Longitudinal Stability And Control Characteristics Of Three Airplane Con- Figurations Downwash And Wake Characteristics At Transonic Speeds Effect Of Stall-control Devices On The Low- Speed Characteristics Of Swept Wings. Part I- Fixed Sweep Effect Of Stall-control Devices On The Low- Speed Characteristics Of Swept Wings. Part Ii- Variable Sweep Effect Of Twist And Camber On The Low-speed Characteristics Of A Swept Wing Preliminary Investigations Of The Effect Of Plan Form Control-surface Characteristics At Transonic Speeds Dynamic Lateral Stability Of Transonic Air- Planes Summary Of Information On Air Inlets- Nose And Wing-root Inlets Diffusers For High-speed Aircraft Analysis Of The Stability Characteristics Of Twin-intake Air-induction Systems Jet Exhaust Characteristics Blade-section Characteristics From Pressure Distributions On The Sections Of Operating Propellers An Experimental Investigation Of Single- Rotation Propeller Characteristics At High- Subsonic Mach Numbers Summary Of Results Of United Aircraft Wind- Tunnel Tests Of A Supersonic Propeller Investigation Of A Dual Propeller At High-Subsonic Mach Numbers Vibration Of Aircraft Propellers Prediction Of First-order Vibratory Stresses For A Propeller Operating In The Flow Field Of A Wing-nacelle-fuselage Combination The Propeller Flutter Problem For High-speed Airplanes

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During the past several years it has been necessary for aeronautical research workers to exert a good portion of their effort in developing the means for conducting research in the high-speed range. The transonic range particularly has presented a very acute problem because of the choking phenomena in wind tunnels at speeds close to the speed of sound. At the same time, the multiplicity of design problems for aircraft introduced by the peculiar flow problems of the transonic speed range has given rise to an enormous demand for detail design data. Substantial progress has been made, however, in developing the required research techniques and in supplying the demand for aerodynamic data required for design purposes. In meeting this demand, it has been necessary to resort to new techniques possessing such novel features that the results obtained have had to be viewed with caution. Furthermore, the kinds of measurements possible with these various techniques are so varied that the correlation of results obtained by different techniques generally becomes an indirect process that can only be accomplished in conjunction with the application of estimates of the extent to which the results of measurements by any given technique are modified by differences that are inherent in the techniques. Thus, in the establishment of the validity and applicability of data obtained by any given technique, direct comparisons between data from different sources are a supplement to but not a substitute for the detailed knowledge required of the characteristics of each technique and fundamental aerodynamic flow phenomena.

“NASA Technical Reports Server (NTRS) 19650074048: NACA Conference On Aerodynamic Problems Of Transonic Airplane Design Introductory Remarks On Transonic Testing Techniques Preliminary Investigation Of Airfoil Charac- Teristics Near M Equals 1 Wing Characteristics Near And At Maximum Lift For Transonic Speeds Status Of The High-speed Flutter Problem The Rolling Power Of Two Wing-aileron Configu- Rations As Affected By Flexibility The Effect Of Aeroelasticity On The Static Longitudinal Stability Of An Example Swept- Wing Bomber Wing Selection As Influenced By The Effect Of Wing Bending On Aerodynamic-center Shift Loss Of Longitudinal Damping In Pitch Due To Flexibility Of Wings In Bending Drag Characteristics At Zero Lift Of Bodies At Transonic Speeds The Flow Over Moderately Swept Wings At High Subsonic Speeds Including The Effects Of Na- Celle Interference Effect On Force Coefficients Of Bodies Of Rev- Olution Attached To Straight And Swept Wings Assessment Of The Drag Problem Design And Calibration Of Airspeed Installa- Tions Stability Some Effects Of Sweepback And Airfoil Thick- Ness On Longitudinal Stability And Control Characteristics At Transonic Speeds A Comparison Of The Longitudinal Stability And Control Characteristics Of Three Airplane Con- Figurations Downwash And Wake Characteristics At Transonic Speeds Effect Of Stall-control Devices On The Low- Speed Characteristics Of Swept Wings. Part I- Fixed Sweep Effect Of Stall-control Devices On The Low- Speed Characteristics Of Swept Wings. Part Ii- Variable Sweep Effect Of Twist And Camber On The Low-speed Characteristics Of A Swept Wing Preliminary Investigations Of The Effect Of Plan Form Control-surface Characteristics At Transonic Speeds Dynamic Lateral Stability Of Transonic Air- Planes Summary Of Information On Air Inlets- Nose And Wing-root Inlets Diffusers For High-speed Aircraft Analysis Of The Stability Characteristics Of Twin-intake Air-induction Systems Jet Exhaust Characteristics Blade-section Characteristics From Pressure Distributions On The Sections Of Operating Propellers An Experimental Investigation Of Single- Rotation Propeller Characteristics At High- Subsonic Mach Numbers Summary Of Results Of United Aircraft Wind- Tunnel Tests Of A Supersonic Propeller Investigation Of A Dual Propeller At High-Subsonic Mach Numbers Vibration Of Aircraft Propellers Prediction Of First-order Vibratory Stresses For A Propeller Operating In The Flow Field Of A Wing-nacelle-fuselage Combination The Propeller Flutter Problem For High-speed Airplanes Introductory Remarks On Transonic Testing Techniques Preliminary Investigation Of Airfoil Charac- Teristics Near M Equals 1 Wing Characteristics Near And At Maximum Lift For Transonic Speeds Status Of The High-speed Flutter Problem The Rolling Power Of Two Wing-aileron Configu- Rations As Affected By Flexibility The Effect Of Aeroelasticity On The Static Longitudinal Stability Of An Example Swept- Wing Bomber Wing Selection As Influenced By The Effect Of Wing Bending On Aerodynamic-center Shift Loss Of Longitudinal Damping In Pitch Due To Flexibility Of Wings In Bending Drag Characteristics At Zero Lift Of Bodies At Transonic Speeds The Flow Over Moderately Swept Wings At High Subsonic Speeds Including The Effects Of Na- Celle Interference Effect On Force Coefficients Of Bodies Of Rev- Olution Attached To Straight And Swept Wings Assessment Of The Drag Problem Design And Calibration Of Airspeed Installa- Tions Stability Some Effects Of Sweepback And Airfoil Thick- Ness On Longitudinal Stability And Control Characteristics At Transonic Speeds A Comparison Of The Longitudinal Stability And Control Characteristics Of Three Airplane Con- Figurations Downwash And Wake Characteristics At Transonic Speeds Effect Of Stall-control Devices On The Low- Speed Characteristics Of Swept Wings. Part I- Fixed Sweep Effect Of Stall-control Devices On The Low- Speed Characteristics Of Swept Wings. Part Ii- Variable Sweep Effect Of Twist And Camber On The Low-speed Characteristics Of A Swept Wing Preliminary Investigations Of The Effect Of Plan Form Control-surface Characteristics At Transonic Speeds Dynamic Lateral Stability Of Transonic Air- Planes Summary Of Information On Air Inlets- Nose And Wing-root Inlets Diffusers For High-speed Aircraft Analysis Of The Stability Characteristics Of Twin-intake Air-induction Systems Jet Exhaust Characteristics Blade-section Characteristics From Pressure Distributions On The Sections Of Operating Propellers An Experimental Investigation Of Single- Rotation Propeller Characteristics At High- Subsonic Mach Numbers Summary Of Results Of United Aircraft Wind- Tunnel Tests Of A Supersonic Propeller Investigation Of A Dual Propeller At High-Subsonic Mach Numbers Vibration Of Aircraft Propellers Prediction Of First-order Vibratory Stresses For A Propeller Operating In The Flow Field Of A Wing-nacelle-fuselage Combination The Propeller Flutter Problem For High-speed Airplanes” Metadata:

  • Title: ➤  NASA Technical Reports Server (NTRS) 19650074048: NACA Conference On Aerodynamic Problems Of Transonic Airplane Design Introductory Remarks On Transonic Testing Techniques Preliminary Investigation Of Airfoil Charac- Teristics Near M Equals 1 Wing Characteristics Near And At Maximum Lift For Transonic Speeds Status Of The High-speed Flutter Problem The Rolling Power Of Two Wing-aileron Configu- Rations As Affected By Flexibility The Effect Of Aeroelasticity On The Static Longitudinal Stability Of An Example Swept- Wing Bomber Wing Selection As Influenced By The Effect Of Wing Bending On Aerodynamic-center Shift Loss Of Longitudinal Damping In Pitch Due To Flexibility Of Wings In Bending Drag Characteristics At Zero Lift Of Bodies At Transonic Speeds The Flow Over Moderately Swept Wings At High Subsonic Speeds Including The Effects Of Na- Celle Interference Effect On Force Coefficients Of Bodies Of Rev- Olution Attached To Straight And Swept Wings Assessment Of The Drag Problem Design And Calibration Of Airspeed Installa- Tions Stability Some Effects Of Sweepback And Airfoil Thick- Ness On Longitudinal Stability And Control Characteristics At Transonic Speeds A Comparison Of The Longitudinal Stability And Control Characteristics Of Three Airplane Con- Figurations Downwash And Wake Characteristics At Transonic Speeds Effect Of Stall-control Devices On The Low- Speed Characteristics Of Swept Wings. Part I- Fixed Sweep Effect Of Stall-control Devices On The Low- Speed Characteristics Of Swept Wings. Part Ii- Variable Sweep Effect Of Twist And Camber On The Low-speed Characteristics Of A Swept Wing Preliminary Investigations Of The Effect Of Plan Form Control-surface Characteristics At Transonic Speeds Dynamic Lateral Stability Of Transonic Air- Planes Summary Of Information On Air Inlets- Nose And Wing-root Inlets Diffusers For High-speed Aircraft Analysis Of The Stability Characteristics Of Twin-intake Air-induction Systems Jet Exhaust Characteristics Blade-section Characteristics From Pressure Distributions On The Sections Of Operating Propellers An Experimental Investigation Of Single- Rotation Propeller Characteristics At High- Subsonic Mach Numbers Summary Of Results Of United Aircraft Wind- Tunnel Tests Of A Supersonic Propeller Investigation Of A Dual Propeller At High-Subsonic Mach Numbers Vibration Of Aircraft Propellers Prediction Of First-order Vibratory Stresses For A Propeller Operating In The Flow Field Of A Wing-nacelle-fuselage Combination The Propeller Flutter Problem For High-speed Airplanes Introductory Remarks On Transonic Testing Techniques Preliminary Investigation Of Airfoil Charac- Teristics Near M Equals 1 Wing Characteristics Near And At Maximum Lift For Transonic Speeds Status Of The High-speed Flutter Problem The Rolling Power Of Two Wing-aileron Configu- Rations As Affected By Flexibility The Effect Of Aeroelasticity On The Static Longitudinal Stability Of An Example Swept- Wing Bomber Wing Selection As Influenced By The Effect Of Wing Bending On Aerodynamic-center Shift Loss Of Longitudinal Damping In Pitch Due To Flexibility Of Wings In Bending Drag Characteristics At Zero Lift Of Bodies At Transonic Speeds The Flow Over Moderately Swept Wings At High Subsonic Speeds Including The Effects Of Na- Celle Interference Effect On Force Coefficients Of Bodies Of Rev- Olution Attached To Straight And Swept Wings Assessment Of The Drag Problem Design And Calibration Of Airspeed Installa- Tions Stability Some Effects Of Sweepback And Airfoil Thick- Ness On Longitudinal Stability And Control Characteristics At Transonic Speeds A Comparison Of The Longitudinal Stability And Control Characteristics Of Three Airplane Con- Figurations Downwash And Wake Characteristics At Transonic Speeds Effect Of Stall-control Devices On The Low- Speed Characteristics Of Swept Wings. Part I- Fixed Sweep Effect Of Stall-control Devices On The Low- Speed Characteristics Of Swept Wings. Part Ii- Variable Sweep Effect Of Twist And Camber On The Low-speed Characteristics Of A Swept Wing Preliminary Investigations Of The Effect Of Plan Form Control-surface Characteristics At Transonic Speeds Dynamic Lateral Stability Of Transonic Air- Planes Summary Of Information On Air Inlets- Nose And Wing-root Inlets Diffusers For High-speed Aircraft Analysis Of The Stability Characteristics Of Twin-intake Air-induction Systems Jet Exhaust Characteristics Blade-section Characteristics From Pressure Distributions On The Sections Of Operating Propellers An Experimental Investigation Of Single- Rotation Propeller Characteristics At High- Subsonic Mach Numbers Summary Of Results Of United Aircraft Wind- Tunnel Tests Of A Supersonic Propeller Investigation Of A Dual Propeller At High-Subsonic Mach Numbers Vibration Of Aircraft Propellers Prediction Of First-order Vibratory Stresses For A Propeller Operating In The Flow Field Of A Wing-nacelle-fuselage Combination The Propeller Flutter Problem For High-speed Airplanes
  • Author: ➤  
  • Language: English

“NASA Technical Reports Server (NTRS) 19650074048: NACA Conference On Aerodynamic Problems Of Transonic Airplane Design Introductory Remarks On Transonic Testing Techniques Preliminary Investigation Of Airfoil Charac- Teristics Near M Equals 1 Wing Characteristics Near And At Maximum Lift For Transonic Speeds Status Of The High-speed Flutter Problem The Rolling Power Of Two Wing-aileron Configu- Rations As Affected By Flexibility The Effect Of Aeroelasticity On The Static Longitudinal Stability Of An Example Swept- Wing Bomber Wing Selection As Influenced By The Effect Of Wing Bending On Aerodynamic-center Shift Loss Of Longitudinal Damping In Pitch Due To Flexibility Of Wings In Bending Drag Characteristics At Zero Lift Of Bodies At Transonic Speeds The Flow Over Moderately Swept Wings At High Subsonic Speeds Including The Effects Of Na- Celle Interference Effect On Force Coefficients Of Bodies Of Rev- Olution Attached To Straight And Swept Wings Assessment Of The Drag Problem Design And Calibration Of Airspeed Installa- Tions Stability Some Effects Of Sweepback And Airfoil Thick- Ness On Longitudinal Stability And Control Characteristics At Transonic Speeds A Comparison Of The Longitudinal Stability And Control Characteristics Of Three Airplane Con- Figurations Downwash And Wake Characteristics At Transonic Speeds Effect Of Stall-control Devices On The Low- Speed Characteristics Of Swept Wings. Part I- Fixed Sweep Effect Of Stall-control Devices On The Low- Speed Characteristics Of Swept Wings. Part Ii- Variable Sweep Effect Of Twist And Camber On The Low-speed Characteristics Of A Swept Wing Preliminary Investigations Of The Effect Of Plan Form Control-surface Characteristics At Transonic Speeds Dynamic Lateral Stability Of Transonic Air- Planes Summary Of Information On Air Inlets- Nose And Wing-root Inlets Diffusers For High-speed Aircraft Analysis Of The Stability Characteristics Of Twin-intake Air-induction Systems Jet Exhaust Characteristics Blade-section Characteristics From Pressure Distributions On The Sections Of Operating Propellers An Experimental Investigation Of Single- Rotation Propeller Characteristics At High- Subsonic Mach Numbers Summary Of Results Of United Aircraft Wind- Tunnel Tests Of A Supersonic Propeller Investigation Of A Dual Propeller At High-Subsonic Mach Numbers Vibration Of Aircraft Propellers Prediction Of First-order Vibratory Stresses For A Propeller Operating In The Flow Field Of A Wing-nacelle-fuselage Combination The Propeller Flutter Problem For High-speed Airplanes Introductory Remarks On Transonic Testing Techniques Preliminary Investigation Of Airfoil Charac- Teristics Near M Equals 1 Wing Characteristics Near And At Maximum Lift For Transonic Speeds Status Of The High-speed Flutter Problem The Rolling Power Of Two Wing-aileron Configu- Rations As Affected By Flexibility The Effect Of Aeroelasticity On The Static Longitudinal Stability Of An Example Swept- Wing Bomber Wing Selection As Influenced By The Effect Of Wing Bending On Aerodynamic-center Shift Loss Of Longitudinal Damping In Pitch Due To Flexibility Of Wings In Bending Drag Characteristics At Zero Lift Of Bodies At Transonic Speeds The Flow Over Moderately Swept Wings At High Subsonic Speeds Including The Effects Of Na- Celle Interference Effect On Force Coefficients Of Bodies Of Rev- Olution Attached To Straight And Swept Wings Assessment Of The Drag Problem Design And Calibration Of Airspeed Installa- Tions Stability Some Effects Of Sweepback And Airfoil Thick- Ness On Longitudinal Stability And Control Characteristics At Transonic Speeds A Comparison Of The Longitudinal Stability And Control Characteristics Of Three Airplane Con- Figurations Downwash And Wake Characteristics At Transonic Speeds Effect Of Stall-control Devices On The Low- Speed Characteristics Of Swept Wings. Part I- Fixed Sweep Effect Of Stall-control Devices On The Low- Speed Characteristics Of Swept Wings. Part Ii- Variable Sweep Effect Of Twist And Camber On The Low-speed Characteristics Of A Swept Wing Preliminary Investigations Of The Effect Of Plan Form Control-surface Characteristics At Transonic Speeds Dynamic Lateral Stability Of Transonic Air- Planes Summary Of Information On Air Inlets- Nose And Wing-root Inlets Diffusers For High-speed Aircraft Analysis Of The Stability Characteristics Of Twin-intake Air-induction Systems Jet Exhaust Characteristics Blade-section Characteristics From Pressure Distributions On The Sections Of Operating Propellers An Experimental Investigation Of Single- Rotation Propeller Characteristics At High- Subsonic Mach Numbers Summary Of Results Of United Aircraft Wind- Tunnel Tests Of A Supersonic Propeller Investigation Of A Dual Propeller At High-Subsonic Mach Numbers Vibration Of Aircraft Propellers Prediction Of First-order Vibratory Stresses For A Propeller Operating In The Flow Field Of A Wing-nacelle-fuselage Combination The Propeller Flutter Problem For High-speed Airplanes” Subjects and Themes:

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Find NASA Technical Reports Server (NTRS) 19650074048: NACA Conference On Aerodynamic Problems Of Transonic Airplane Design Introductory Remarks On Transonic Testing Techniques Preliminary Investigation Of Airfoil Charac- Teristics Near M Equals 1 Wing Characteristics Near And At Maximum Lift For Transonic Speeds Status Of The High-speed Flutter Problem The Rolling Power Of Two Wing-aileron Configu- Rations As Affected By Flexibility The Effect Of Aeroelasticity On The Static Longitudinal Stability Of An Example Swept- Wing Bomber Wing Selection As Influenced By The Effect Of Wing Bending On Aerodynamic-center Shift Loss Of Longitudinal Damping In Pitch Due To Flexibility Of Wings In Bending Drag Characteristics At Zero Lift Of Bodies At Transonic Speeds The Flow Over Moderately Swept Wings At High Subsonic Speeds Including The Effects Of Na- Celle Interference Effect On Force Coefficients Of Bodies Of Rev- Olution Attached To Straight And Swept Wings Assessment Of The Drag Problem Design And Calibration Of Airspeed Installa- Tions Stability Some Effects Of Sweepback And Airfoil Thick- Ness On Longitudinal Stability And Control Characteristics At Transonic Speeds A Comparison Of The Longitudinal Stability And Control Characteristics Of Three Airplane Con- Figurations Downwash And Wake Characteristics At Transonic Speeds Effect Of Stall-control Devices On The Low- Speed Characteristics Of Swept Wings. Part I- Fixed Sweep Effect Of Stall-control Devices On The Low- Speed Characteristics Of Swept Wings. Part Ii- Variable Sweep Effect Of Twist And Camber On The Low-speed Characteristics Of A Swept Wing Preliminary Investigations Of The Effect Of Plan Form Control-surface Characteristics At Transonic Speeds Dynamic Lateral Stability Of Transonic Air- Planes Summary Of Information On Air Inlets- Nose And Wing-root Inlets Diffusers For High-speed Aircraft Analysis Of The Stability Characteristics Of Twin-intake Air-induction Systems Jet Exhaust Characteristics Blade-section Characteristics From Pressure Distributions On The Sections Of Operating Propellers An Experimental Investigation Of Single- Rotation Propeller Characteristics At High- Subsonic Mach Numbers Summary Of Results Of United Aircraft Wind- Tunnel Tests Of A Supersonic Propeller Investigation Of A Dual Propeller At High-Subsonic Mach Numbers Vibration Of Aircraft Propellers Prediction Of First-order Vibratory Stresses For A Propeller Operating In The Flow Field Of A Wing-nacelle-fuselage Combination The Propeller Flutter Problem For High-speed Airplanes Introductory Remarks On Transonic Testing Techniques Preliminary Investigation Of Airfoil Charac- Teristics Near M Equals 1 Wing Characteristics Near And At Maximum Lift For Transonic Speeds Status Of The High-speed Flutter Problem The Rolling Power Of Two Wing-aileron Configu- Rations As Affected By Flexibility The Effect Of Aeroelasticity On The Static Longitudinal Stability Of An Example Swept- Wing Bomber Wing Selection As Influenced By The Effect Of Wing Bending On Aerodynamic-center Shift Loss Of Longitudinal Damping In Pitch Due To Flexibility Of Wings In Bending Drag Characteristics At Zero Lift Of Bodies At Transonic Speeds The Flow Over Moderately Swept Wings At High Subsonic Speeds Including The Effects Of Na- Celle Interference Effect On Force Coefficients Of Bodies Of Rev- Olution Attached To Straight And Swept Wings Assessment Of The Drag Problem Design And Calibration Of Airspeed Installa- Tions Stability Some Effects Of Sweepback And Airfoil Thick- Ness On Longitudinal Stability And Control Characteristics At Transonic Speeds A Comparison Of The Longitudinal Stability And Control Characteristics Of Three Airplane Con- Figurations Downwash And Wake Characteristics At Transonic Speeds Effect Of Stall-control Devices On The Low- Speed Characteristics Of Swept Wings. Part I- Fixed Sweep Effect Of Stall-control Devices On The Low- Speed Characteristics Of Swept Wings. Part Ii- Variable Sweep Effect Of Twist And Camber On The Low-speed Characteristics Of A Swept Wing Preliminary Investigations Of The Effect Of Plan Form Control-surface Characteristics At Transonic Speeds Dynamic Lateral Stability Of Transonic Air- Planes Summary Of Information On Air Inlets- Nose And Wing-root Inlets Diffusers For High-speed Aircraft Analysis Of The Stability Characteristics Of Twin-intake Air-induction Systems Jet Exhaust Characteristics Blade-section Characteristics From Pressure Distributions On The Sections Of Operating Propellers An Experimental Investigation Of Single- Rotation Propeller Characteristics At High- Subsonic Mach Numbers Summary Of Results Of United Aircraft Wind- Tunnel Tests Of A Supersonic Propeller Investigation Of A Dual Propeller At High-Subsonic Mach Numbers Vibration Of Aircraft Propellers Prediction Of First-order Vibratory Stresses For A Propeller Operating In The Flow Field Of A Wing-nacelle-fuselage Combination The Propeller Flutter Problem For High-speed Airplanes at online marketplaces:


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