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Primary view of The Aerodynamic Wind Vane and the Inherent Stability of Airplanes
Lapresle, A.
February 1931
Primary view of Effects of leading-edge radius on the longitudinal stability of two 45 degree sweptback wings as influenced by Reynolds numbers up to 8.20 x 10(exp 6) and Mach numbers up to 0.303
Foster, Gerald V. & Schneider, William C.
July 28, 1955
Primary view of A flight investigation at transonic speeds and small angles of attack of the aerodynamic characteristics of a model having a 45 degree sweptback wing of aspect ratio 3 with an Naca 64A006 airfoil section
Holdaway, George H.
January 25, 1954
Primary view of Charts for estimating tail-rotor contribution to helicopter directional stability and control in low-speed flight
Amer, Kenneth B. & Gessow, Alfred
October 27, 1953
Primary view of Studies of the speed stability of a tandem helicopter in forward flight
Tapscott, Robert J. & Amer, Kenneth B.
June 4, 1953
Primary view of Measurement of the moments of inertia of an airplane by a simplified method
Turner, Howard L.
October 1950
Primary view of An introduction to the physical aspects of helicopter stability
Gessow, Alfred & Amer, Kenneth B.
November 1949
Primary view of Inherent Stability of Helicopters
Crocco, G. Arturo
October 1923
Primary view of A method for estimating variations in the roots of the lateral-stability quartic due to changes in mass and aerodynamic parameters of an airplane
Gates, Ordway B., Jr. & Woodling, C. H.
January 1954
Primary view of A method for measuring the product of inertia and the inclination of the principal longitudinal axis of inertia of an airplane
Boucher, Robert W.; Rich, Drexel A.; Crane, Harold L. & Matheny, Cloyce E.
April 1954
Primary view of Summary of the theoretical lift, damping-in-roll, and center-of-pressure characteristics of various wing plan forms at supersonic speeds
Piland, Robert O.
October 1949
Primary view of A Comparison of Predicted and Experimentally Determined Longitudinal Dynamic Responses of a Stabilized Airplane
Smaus, Louis H.; Gore, Marvin R. & Waugh, Merle G.
December 1951
Primary view of The motions of rolling symmetrical missiles referred to a body-axis system
Nelson, Robert L.
November 1956
Primary view of Effect of fuselage and tail surfaces on low-speed yawing characteristics of a swept-wing model as determined in curved-flow test section of Langley stability tunnel
Bird, John D.; Jaquet, Byron M. & Cowan, John W.
October 1951
Primary view of A simplified method for the determination and analysis of the neutral-lateral-oscillatory-stability boundary
Sternfield, Leonard & Gates, Ordway B., Jr.
October 1948
Primary view of Hovering and Low-Speed Performance and Control Characteristics of an Aerodynamic-Servocontrolled Helicopter Rotor System as Determined on the Langley Helicopter Tower
Carpenter, Paul J. & Paulnock, Russell S.
May 1950
Primary view of New Lateral Stabilizing Device for Airplanes
Constantin, Louis
January 1921
Primary view of The Development of Cambered Airfoil Sections Having Favorable Lift Characteristics at Supercritical Mach Numbers
Graham, Donald J.
December 1948
Primary view of Tests to Determine Effects of Slipstream Rotation on the Lateral Stability Characteristics of a Single-Engine Low-Wing Aircraft Model
Purser, Paul E. & Spear, Margaret F.
September 1946
Primary view of Flight, Analog-Simulator, and Analytical Studies of an Automatically Controlled Interceptor Which Uses a Bank-Angle-Error Computer for Lateral Commands
Cheatham, Donald C. & Brissenden, Roy F.
August 11, 1958
Primary view of Static stability of seaplane floats and hulls
Diehl, W. S.
March 1924
Primary view of A Study of Static Stability of Airships
Rizzo, Frank
September 1924
Primary view of Investigation at a Mach Number of 1.93 to Determine Lift, Drag, Pitching-Moment, and Average Downwash Characteristics for Several Missile Configurations Having Rectangular Wings and Tails of Various Spans
Grigsby, Carl E.
October 19, 1950
Primary view of Low-speed lateral stability and aileron-effectiveness characteristics at a Reynolds number of 3.5 x 10(exp 6) of a wing with leading-edge sweepback decreasing from 45 degrees at the root to 20 degrees at the tip
Lange, Roy H. & McLemore, Huel C.
July 6, 1950
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