Technical Report Archive & Image Library (TRAIL) - 1,166 Matching Results

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Primary view of The 1000 HP Traffic Airplane of the Zeppelin Works in Staaken
Rohrbach, A. K.
September 1921
Primary view of The A.B.C. "Robin" (British): A Single-Seat Cabin Monoplane
A. B. C. Motors
September 1929
Primary view of Acceleration Measurements During Landings of a 1/5.5-Size Dynamic Model of the Columbia XJL-1 Amphibian in Smooth Water and in Waves: Langley Tank Model 208M, TED No. NACA 2336
Clement, Eugene P. & Havens, Robert F.
September 25, 1947
Primary view of Adaptation of a Cascade Impactor to Flight Measurement of Droplet Size in Clouds
Levine, Joseph & Kleinknecht, Kenneth S.
September 18, 1951
Primary view of Additional results of an investigation at transonic speeds to determine the effects of a heated propulsive jet on the drag characteristics of a series of related afterbodies
Henry, Beverly Z., Jr. & Cahn, Maurice S.
September 24, 1956
Primary view of Aerodynamic and Hydrodynamic Tests of a Family of Models of Flying-Boat Hulls Derived From a Streamline Body: NACA Model 84 Series
Parkinson, John B.; Olson, Roland E.; Draley, Eugene C. & Luoma, Arvo A.
September 1943
Primary view of Aerodynamic characteristics and pressure distributions of a 6-percent-thick 49 degree sweptback wing with blowing over half-span and full-span flaps
Whittle, Edward F., Jr. & McLemore, H. Clyde
September 20, 1955
Primary view of Aerodynamic characteristics at Mach numbers from 0.7 to 1.75 of a four-engine swept-wing airplane configuration as obtained from a rocket-propelled model test
Chapman, Rowe, Jr.
September 2, 1955
Primary view of Aerodynamic Characteristics at Mach Numbers From 2.5 to 3.5 of a Canard Bomber Configuration Designed for Supersonic Cruise Flight
Carmel, Melvin M.; Kelly, Thomas C. & Gregory, Donald T.
September 10, 1958
Primary view of Aerodynamic characteristics at transonic speeds of a 60 degree delta wing equipped with a constant-chord flap-type control with and without an unshielded horn balance: transonic-bump method
Wiley, Harleth G. & Zontek, Leon
September 16, 1952
Primary view of The Aerodynamic Characteristics at Transonic Speeds of an All-Movable, Tapered, 45 Degree Sweptback, Aspect-Ratio-4 Tail Deflected About a Skewed Hinge Axis and Equipped with an Inset Unbalancing Tab
Watson, James M.
September 29, 1953
Primary view of Aerodynamic Characteristics of a 0.5-Scale Model of the Fairchild XSAM-N-2 Lark Missile at High Subsonic Speeds
Martin, Andrew & Hunter, Harlo A.
September 28, 1949
Primary view of Aerodynamic Characteristics of a 0.04956-Scale Model of the Convair F-102A Airplane at Mach Numbers of 1.41, 1.61, and 2.01
Spearman, M. Leroy & Driver, Cornelius
September 30, 1955
Primary view of Aerodynamic characteristics of a two-blade NACA 10-(3)(08)-03R propeller
Evans, Albert J. & Salters, Leland B., Jr.
September 2, 1948
Primary view of Aerodynamic characteristics of a wing with quarter-chord line swept back 60 degrees, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section: transonic-bump method
King, Thomas J., Jr. & Myers, Boyd C., II
September 6, 1949
Primary view of Aerodynamic Characteristics of Airfoils 4: Continuation of Reports Nos. 93, 124, and 182
unknown creator
September 1926
Primary view of Aerodynamic Characteristics of an Airfoil-Forebody Swept Flying-Boat Hull With a Wing and Tail Swept Back 51.3 Degrees at the Leading Edge
Naeseth, Rodger L. & MacLeod, Richard G.
September 9, 1949
Primary view of Aerodynamic Characteristics of Four Republic Airfoil Sections from Tests in Langley Two-Dimensional Low-Turbulence Tunnels
Klein, Milton M.
September 27, 1945
Primary view of Aerodynamic Characteristics of the NACA 747A315 and 747A415 Airfoils From Tests in the NACA Two-Dimensional Low-Turbulence Pressure Tunnel
von Doenhoff, Albert E. & Stivers, Louis S., Jr.
September 1944
Primary view of Aerodynamic characteristics of the NACA RM-10 research missile in the Ames 1- by 3-foot supersonic wind tunnel no. 2: Pressure and force measurements at Mach numbers of 1.52 and 1.98
Perkins, Edward W.; Gowen, Forrest E. & Jorgensen, Leland H.
September 19, 1951
Primary view of Aerodynamic Computation of Gliders
Schrenk, M.
September 1922
Primary view of The aerodynamic forces and moments on a 1/10-scale model of a fighter airplane in spinning attitudes as measured on a rotary balance in the Langley 20-foot free-spinning tunnel
Stone, Ralph W., Jr.; Burk, Sanger M., Jr. & Bihrle, William, Jr.
September 1950
Primary view of Aerodynamic heat transfer and zero-lift of a flat windshield canopy on the NACA RM-10 research vehicle at high Reynolds numbers for a flight Mach number range from 1.5 to 3.0
Hoffman, Sherwood & Chauvin, Leo T.
September 26, 1956
Primary view of Aerodynamic heating of a wing as determined from a free-flight rocket-model test to Mach number 3.64
Swanson, Andrew G. & Rumsey, Charles B.
September 11, 1956
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