Technical Report Archive & Image Library (TRAIL) - 5,157 Matching Results

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Primary view of Aerodynamic and hydrodynamic characteristics of a deck-inlet multijet water-based-aircraft configuration designed for supersonic flight
Bielat, Ralph P.; Coffee, Claude W., Jr. & Petynia, William W.
December 5, 1956
Primary view of Aerodynamic and hydrodynamic characteristics of a proposed supersonic multijet water-based hydro-ski aircraft with a variable-incidence wing
Petynia, William W.; Hasson, Dennis F. & Spooner, Stanley H.
October 23, 1957
Primary view of Aerodynamic and hydrodynamic characteristics of models of some aircraft-towed mine-sweeping devices : TED No. NACA AR 8201
Shanks, Robert E.
December 1, 1955
Primary view of Aerodynamic and inlet-flow-field characteristics at a free-stream Mach number of 3.0 for airplanes with circular fuselage cross sections and for two engine locations
Dryer, Murray & Luidens, Roger W.
March 18, 1958
Primary view of Aerodynamic and Lateral-Control Characteristics of a 1/28-Scale Model of the Bell X-1 Airplane Wing-Fuselage Combination: Transonic-Bump Method
Lockwood, Vernard E.
May 5, 1950
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 a Mach Number of 1.25 of a 6-Percent-Thick Triangular Wing and 6- and 9-Percent-Thick Triangular Wings in Combination With a Fuselage: Wing Aspect Ratio 2.31, Biconvex Airfoil Sections
Hall, Albert W. & Morris, Garland J.
May 5, 1950
Primary view of Aerodynamic Characteristics at a Mach Number of 1.38 of Four Wings of Aspect Ratio 4 Having Quarter-Chord Sweep Angles of 0 Degrees, 35 Degrees, 45 Degrees, and 60 Degrees
Kemp, William B., Jr.; Goodson, Kenneth W. & Booth, Robert A.
October 10, 1950
Primary view of Aerodynamic Characteristics at a Mach Number of 6.8 of Two Hypersonic Missile Configurations, One With Low-Aspect-Ratio Cruciform Fins and Trailing-Edge Flaps and One With a Flared Afterbody and All-Movable Controls
Robinson, Ross B. & Bernot, Peter T.
August 4, 1958
Primary view of Aerodynamic Characteristics at a Mach Number of 6.8 of Two Hypersonic Missile Configurations, One With Low-Aspect-Ratio Cruciform Fins and Trailing-Edge Flaps and One With a Flared Afterbody and All-Movable Controls
Robinson, Ross B. & Bernot, Peter T.
August 4, 1958
Primary view of Aerodynamic characteristics at high and low subsonic Mach numbers of four NACA 6-series airfoil sections at angles of attack from -2 to 31 degrees
Wilson, Homer B., Jr. & Horton, Elmer A.
June 5, 1953
Primary view of Aerodynamic Characteristics at High and Low Subsonic Mach Numbers of the NACA 0012, 64₂-015, and 64₃-018 Airfoil Sections at Angles of Attack from -2 Degrees to 30 Degrees
Critzos, Chris C.
July 23, 1954
Primary view of Aerodynamic characteristics at high speeds of a two-blade NACA 10-(3)(062)-045 propeller and of a two-blade NACA 10-(3)(08)-045 propeller
Solomon, William
October 1, 1948
Primary view of Aerodynamic characteristics at high speeds of full-scale propellers having Clark Y blade sections
Johnson, Peter J.
October 26, 1948
Primary view of Aerodynamic Characteristics at High Speeds of Full-Scale Propellers Having Different Shank Designs
Maynard, Julian D.
February 13, 1947
Primary view of Aerodynamic characteristics at Mach number 4.04 of a rectangular wing of aspect ratio 1.33 having a 6-percent-thick circular-arc profile and a 30-percent-chord full-span trailing-edge flap
Dunning, Robert W. & Ulmann, Edward F.
May 29, 1953
Primary view of Aerodynamic characteristics at Mach number of 2.01 of two cruciform missile configurations having 70 degree delta wings with length-diameter ratios of 14.8 and 17.7 with several canard controls
Spearman, M. Leroy & Robinson, Ross B.
August 30, 1954
Primary view of Aerodynamic characteristics at Mach number of 4.06 of a typical supersonic airplane model using body and vertical-tail wedges to improve directional stability
Dunning, Robert W.
December 3, 1957
Primary view of Aerodynamic characteristics at Mach numbers 2.36 and 2.87 of an airplane configuration having a cambered arrow wing with a 75 degree swept leading edge
Hallissy, Joseph M., Jr. & Hasson, Dennis F.
August 4, 1958
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 Mach Numbers of 1.61 and 2.01 of Various Tip Controls on the Wing Panel of a 0.05-Scale Model of a Martin XASM-N-7 (Bullpup) Missile: TED No. NACA AD 3106
Driver, Cornelius
1956~
Primary view of Aerodynamic characteristics at subcritical and supercritical Mach numbers of two airfoil sections having sharp leading edges and extreme rearward positions of maximum thickness
Eggers, A. J., Jr.
November 6, 1947
Primary view of Aerodynamic characteristics at subsonic and supersonic Mach numbers of a thin triangular wing of aspect ratio 2 1: maximum thickness at 20 percent of the chord
Berggren, Robert E. & Summers, James L.
November 19, 1948
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