Calculated normal load factors on light airplanes traversing the trailing vortices of heavy transport airplanes /

Random deviations from cruise altitudes of a turbojet transport transport at altitudes between 20,000 and 41,000 feet. /

Gracey, William
Shipp, Jo Ann.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aircraft; Aircraft safety and noise; Piloting; Vehicle Performance.Includes...

Investigation at transonic speeds of the loading over a 40 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2 and NACA 65A004 airfoil sections /

Runckel, Jack F.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aircraft; Stresses and loads.Includes bibliographical...

Aerodynamic loads on an isolated shrouded-propeller configuration of angles of attack from -10 degrees to 110 degrees /

Grunwald, Kalman J.
Goodson, Kenneth W.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Aircraft; Propulsion systems, air-jet.Includes bi...

An investigation of wing and aileron loads due to deflected inboard and outboard ailerons on a 4-percent-thick 30 degree swepptback wing at transonic speeds

Whitcomb, Charles F.
Critzos, Chris C.
Brown, Philippa F.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Aircraft; Stability and control; Stresses and loa...

Flight investigation of some effects of a vane-controlled gust-alleviation system on the wing and tail loads fo a transport airplane /

Schott, Russell L.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Aircraft; Aircraft safety and noise; Piloting; St...

Aerodynamic loads at mach numbers from 0.70 to 2.22 on an airplane model having a wing and canard of triangular plan form and either single or twin vertical tails /

Peterson, Victor L.
Menees, Gene P.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical referenc...

Structural-loads surveys on two tilt-wing VTOL configurations /

Ward, John F.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aircraft; Stresses and loads.Includes bibliographical references.Mode of ac...

Fatigue investigation of full-scale transport-airplane wings tests with constant-amplitude and variable amplitude loading schedules/

Foster, Lee R.
Whlaey, Richard E.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Stresses and loads.Includes bibliographical references.Mode of access: In...

Experimental and calculated flow fields produced by airplanes flying at supersonic speeds /

Smith, Harriet J.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics aircraft; Aircraft safety and noise.Includes bibliographica...

Operational experiences of turbine-powered commercial transport airplanes /

United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aircraft; Aircraft safety and noise; Piloting; Stresses and loads; Struct...

Skid landings of airplanes on rocker-type fuselages. /

Mayo, Wilbur L.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aircraft; Aircraft safety and noise; Stresses and loads.Includes bibliographi...

Aerodynamic load measurements and opening characteristics of automatic leading-edge slats on a 45 degree sweptback wing at transonic speeds /

Arabian, Donald D.
Reid, Charles F.
Runckel, Jack F.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aircraft; Stresses and loads.Includes bibliographical references.Mode o...

An investigation of landing-contact conditions for a large turbojet transport during routine daylight operations /

Stickle, Joseph W.
Silsby, Norman S.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aircraft safety and noise; Structures; Vehicle performance.Includes bibli...

Flight investigation using variable-stability airplanes of minimum stability requirements for high-speed, high-altitude vehicles /

McFadden, Norman M.
Heinle, Donovan R.
Vomaske, Richard F.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Piloting; Stability and control; Vehicle ...

Aerodynamic characteristics of parachutes at mach numbers from 1.6 to 3 /

Maynard, Julian D.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aircraft safety and noise.Includes bibliographical references.Mode of access:...

Random deviations from cruise altitudes of a turbojet transport transport at altitudes between 20,000 and 41,000 feet. /

Gracey, William
Shipp, Jo Ann.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aircraft; Aircraft safety and noise; Piloting; Vehicle Performance.Includes...

Investigation at transonic speeds of the loading over a 40 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2 and NACA 65A004 airfoil sections /

Runckel, Jack F.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aircraft; Stresses and loads.Includes bibliographical...

Aerodynamic loads on an isolated shrouded-propeller configuration of angles of attack from -10 degrees to 110 degrees /

Grunwald, Kalman J.
Goodson, Kenneth W.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Aircraft; Propulsion systems, air-jet.Includes bi...

An investigation of wing and aileron loads due to deflected inboard and outboard ailerons on a 4-percent-thick 30 degree swepptback wing at transonic speeds

Whitcomb, Charles F.
Critzos, Chris C.
Brown, Philippa F.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Aircraft; Stability and control; Stresses and loa...

Flight investigation of some effects of a vane-controlled gust-alleviation system on the wing and tail loads fo a transport airplane /

Schott, Russell L.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Aircraft; Aircraft safety and noise; Piloting; St...

Aerodynamic loads at mach numbers from 0.70 to 2.22 on an airplane model having a wing and canard of triangular plan form and either single or twin vertical tails /

Peterson, Victor L.
Menees, Gene P.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical referenc...

Structural-loads surveys on two tilt-wing VTOL configurations /

Ward, John F.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aircraft; Stresses and loads.Includes bibliographical references.Mode of ac...

Fatigue investigation of full-scale transport-airplane wings tests with constant-amplitude and variable amplitude loading schedules/

Foster, Lee R.
Whlaey, Richard E.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Stresses and loads.Includes bibliographical references.Mode of access: In...

Experimental and calculated flow fields produced by airplanes flying at supersonic speeds /

Smith, Harriet J.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics aircraft; Aircraft safety and noise.Includes bibliographica...

Operational experiences of turbine-powered commercial transport airplanes /

United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aircraft; Aircraft safety and noise; Piloting; Stresses and loads; Struct...

Skid landings of airplanes on rocker-type fuselages. /

Mayo, Wilbur L.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aircraft; Aircraft safety and noise; Stresses and loads.Includes bibliographi...

Aerodynamic load measurements and opening characteristics of automatic leading-edge slats on a 45 degree sweptback wing at transonic speeds /

Arabian, Donald D.
Reid, Charles F.
Runckel, Jack F.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aircraft; Stresses and loads.Includes bibliographical references.Mode o...

An investigation of landing-contact conditions for a large turbojet transport during routine daylight operations /

Stickle, Joseph W.
Silsby, Norman S.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aircraft safety and noise; Structures; Vehicle performance.Includes bibli...

Flight investigation using variable-stability airplanes of minimum stability requirements for high-speed, high-altitude vehicles /

McFadden, Norman M.
Heinle, Donovan R.
Vomaske, Richard F.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Piloting; Stability and control; Vehicle ...

Aerodynamic characteristics of parachutes at mach numbers from 1.6 to 3 /

Maynard, Julian D.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aircraft safety and noise.Includes bibliographical references.Mode of access:...

Random deviations from cruise altitudes of a turbojet transport transport at altitudes between 20,000 and 41,000 feet. /

Gracey, William
Shipp, Jo Ann.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aircraft; Aircraft safety and noise; Piloting; Vehicle Performance.Includes...

Investigation at transonic speeds of the loading over a 40 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2 and NACA 65A004 airfoil sections /

Runckel, Jack F.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aircraft; Stresses and loads.Includes bibliographical...

Aerodynamic loads on an isolated shrouded-propeller configuration of angles of attack from -10 degrees to 110 degrees /

Grunwald, Kalman J.
Goodson, Kenneth W.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Aircraft; Propulsion systems, air-jet.Includes bi...

Calculated normal load factors on light airplanes traversing the trailing vortices of heavy transport airplanes /

Abstract

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Calculated normal load factors on light airplanes traversing the trailing vortices of heavy transport airplanes /

Abstract

Extracted data

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