Technical Report Archive & Image Library (TRAIL) - 208 Matching Results

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Primary view of Development of a new flutter testing technique using a towed dynamic airplane model equipped with an automatic stabilizing system: Experimental and calculated dynamic stability characteristics for speeds up to 200 mph
Schneider, William C.
March 25, 1955
Primary view of Lift, drag, and static longitudinal stability characteristics of four airplane-like configurations at Mach numbers from 3.00 to 6.28
Neice, Stanford E.; Wong, Thomas J. & Hermach, Charles A.
April 25, 1955
Primary view of Effect of inlet-air-flow-distortions on steady-state performance of J65-B-3 turbojet engine
Smith, Ivan D.; Braithwaite, W. M. & Calvert, Howard F.
January 25, 1956
Primary view of Experimental investigation of effect of cooling air on turbine performance of two turbojet engines modified for air-cooling
Smith, Gordon T.; Freche, John C. & Cochran, Reeves P.
January 25, 1956
Primary view of Investigation of the effects of body indentation and of wing-plan-form modification on the longitudinal characteristics of a 60 degree swept-wing-body combination at Mach numbers of 1.41, 1.61, and 2.10
Sevier, John R., Jr.
July 25, 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 Investigation of Two Short Annular Diffuser Configurations Utilizing Section and Injection as a Means of Boundary-Layer Control
Wilbur, Langley W. & Higginbotham, James T.
January 25, 1955
Primary view of Forces and moments on inclined bodies at Mach numbers from 3.0 to 6.3
Dennis, David H. & Cunningham, Bernard E.
June 25, 1954
Primary view of Interference effects at Mach 1.9 on a horizontal tail due to trailing shock waves from an axisymmetric body with an exiting jet
Salmi, Reino J. & Klann, John L.
January 25, 1956
Primary view of Preliminary Free-Flight Investigation of the Effect of Airfoil Section on Aileron Rolling Effectiveness at Transonic and Supersonic Speeds
Sandahl, Carl A.
June 25, 1948
Primary view of Free-Flight Investigation at Transonic and Supersonic Speeds of the Rolling Effectiveness of a 42.7 Degree Sweptback Wing Having Partial-Span Ailerons
Sandahl, Carl A.
October 25, 1948
Primary view of NACA Transonic Wing-Tunnel Test Sections
Wright, Ray H. & Ward, Vernon G.
October 25, 1948
Primary view of Preliminary Investigation at a Mach Number of 1.9 and a Reynolds Number of 2,200,000 of Three Ailerons Applicable to the Bell XS-2 Airplane Design
Sivells, James C. & Conner, D. William
May 25, 1948
Primary view of Experimental investigation of the drag of 30 degree, 60 degree, and 90 degree cone cylinders at Mach numbers between 1.5 and 8.2
Seiff, Alvin & Sommer, Simon C.
April 25, 1952
Primary view of Investigation of Stresses Due to Thermal Gradients in Typical Aircraft Structures
Barzelay, Martin E. & Boison, James C.
January 25, 1952
Primary view of Flight Investigation of the Longitudinal Stability and Control Characteristics of the Douglas D-558-I Airplane (BuAero No. 37972) at Mach Numbers Up to 0.89
Sadoff, Melvin; Roden, William S. & Eggleston, John M.
June 25, 1951
Primary view of A study of the flow over a 45 degree sweptback wing-fuselage combination at transonic Mach numbers
Whitcomb, Richard T. & Kelly, Thomas C.
June 25, 1952
Primary view of Total-Pressure Recovery of a Circular Underslung Inlet With Three Different Nose Shapes at a Mach Number of 1.42
Merlet, Charles F. & Carter, Howard S.
February 25, 1952
Primary view of The effect of bluntness on the drag of spherical-tipped truncated cones of fineness ratio 3 at Mach numbers 1.2 to 7.4
Sommer, Simon C. & Stark, James A.
April 25, 1952
Primary view of Effects of Propeller-Shank Geometry and Propeller-Spinner-Juncture Configuration on Characteristics of an NACA 1-Series Cowling-Spinner Combination With an Eight-Blade Dual-Rotation Propeller
Keith, Arvid L., Jr.; Bingham, Gene J. & Rubin, Arnold J.
September 25, 1951
Primary view of A flight study of requirements for satisfactory lateral oscillatory characteristics of fighter aircraft
Liddell, Charles J., Jr.; Creer, Brent Y. & Van Dyke, Rudolph D., Jr.
July 25, 1951
Primary view of Flight calibration of angle-of-attack and sideslip detectors on the fuselage of a 35 degree swept-wing fighter airplane
McFadden, Norman M.; Bray, Richard S. & Rathert, George A., Jr.
February 25, 1952
Primary view of Free-flight investigation of longitudinal stability and control of a rocket-propelled missile model having cruciform, triangular, inline wings and tails
Hall, James R.
March 25, 1952
Primary view of The Ames supersonic free-flight wind tunnel
Seiff, Alvin; James, Carlton S.; Canning, Thomas N. & Boissevain, Alfred G.
April 25, 1952
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