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Primary view of Inverness: Socioeconomic Features
U.S. Fish and Wildlife Service
1984
Primary view of Inverness: Soils and Landforms
U.S. Fish and Wildlife Service
1984
Primary view of Investigation and Preparation of Polymer Films to Improve the Separation of Water and Salts in Saline Water Conversion
Monsanto Research Corporation
December 1962
Primary view of Investigation at a Mach Number of 1.2 of Two 45 Degree Sweptback Wings Utilizing NACA 2-006 and NACA 65A006 Airfoil Sections
Wilson, Homer B., Jr.
September 11, 1952
Primary view of Investigation at a Mach number of 1.90 of a diverter-type boundary-layer removal system for a scoop inlet
Kochendorfer, Fred D.
June 8, 1953
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 Investigation at high and low subsonic Mach numbers of two symmetrical 6-percent-thick airfoil sections designed to have high maximum lift coefficients at low speeds
Paradiso, Nicholas J.
October 17, 1952
Primary view of Investigation at high subsonic speeds of a 45 sweptback horizontal tail with plain and horn-balanced control surfaces
Johnson, Harold S. & Thompson, Robert F.
March 31, 1950
Primary view of Investigation at high subsonic speeds of a body-contouring method for alleviating the adverse interference at the root of a sweptback wing
McDevitt, John B. & Haire, William M.
April 1956
Primary view of Investigation at high subsonic speeds of bodies mounted from the wing of an unswept-wing-fuselage model, including measurements of body loads
Silvers, H. Norman & King, Thomas J., Jr.
November 14, 1952
Primary view of Investigation at high subsonic speeds of finned and unfinned bodies mounted at various locations from the wings of unswept- and swept-wing--fuselage models, including measurements of body loads
Alford, William J., Jr. & Silvers, H. Norman
April 1, 1954
Primary view of Investigation at High Subsonic Speeds of Methods of Alleviating the Adverse Interference at the Root of a Swept-Back Wing
Boddy, Lee E.
August 10, 1950
Primary view of Investigation at high subsonic speeds of some effects of sideslip on the aerodynamic loads on finned and unfinned bodies mounted from the wing of a swept-wing-fuselage model
King, Thomas J., Jr.
April 26, 1956
Primary view of Investigation at high subsonic speeds of the effect of adding various combinations of missiles on the aerodynamic characteristics of sweptback and unswept wings combined with a fuselage
Silvers, H. Norman & Alford, William J., Jr.
June 24, 1954
Primary view of An investigation at high subsonic speeds of the effects of horizontal-tail height on the aerodynamic and loading characteristics in sideslip on a 45 degree sweptback, untapered tail assembly as determined from force tests and integrated vertical-tail span loadings
Wiley, Harleth G. & Moseley, William C., Jr.
June 28, 1955
Primary view of Investigation at High Subsonic Speeds of the Effects of Various Horizontal Fuselage Forebody Fins on the Directional and Longitudinal Stability of a Complete Model Having a 45 Degree Sweptback Wing
Sleeman, William C., Jr.
January 16, 1957
Primary view of Investigation at high subsonic speeds of the effects of various underwing external-store arrangements on the aerodynamic characteristics of a 1/16-scale model of the Douglas D-558-II Research Airplane
Silvers, H. Norman & King, Thomas J., Jr.
July 18, 1955
Primary view of Investigation at high subsonic speeds of the pressure distributions on a 45 degree sweptback horizontal tail mounted at 50-percent and 100-percent vertical-tail span
Wiley, Harleth G. & Moseley, William C., Jr.
November 24, 1954
Primary view of An investigation at high subsonic speeds of the pressure distributions on a 45 degree sweptback vertical tail in sideslip with and without a 45 degree sweptback horizontal tail located on the fuselage center line
Wiley, Harleth G. & Moseley, William C., Jr.
November 2, 1954
Primary view of Investigation at high subsonic speeds of the static lateral and directional stability and tail-loads characteristics of a model having a highly tapered swept wing of aspect ratio 3 and two horizontal-tail positions
Few, Albert G., Jr.
September 11, 1956
Primary view of Investigation at High Subsonic Speeds of the Static Longitudinal and Lateral Stability Characteristics of Two Canard Airplane Configurations
Sleeman, William C., Jr.
December 3, 1957
Primary view of Investigation at High Subsonic Speeds of the Use of Low Auxiliary Tail Surfaces Having Dihedral to Improve the Longitudinal and Directional Stability of a T-Tail Model at High Lift
Sleeman, William C., Jr.
December 5, 1957
Primary view of Investigation at large scale of the pressure distribution and flow phenomena over a wing with the leading edge swept back 47.5 degrees having circular-arc airfoil sections and equipped with drooped-nose and plain flaps
Lange, Roy H.; Whittle, Edward F., Jr. & Fink, Marvin P.
September 8, 1949
Primary view of Investigation at Low Speed of 45 Degrees and 60 Degrees Sweptback, Tapered, Low-Drag Wings Equipped With Various Types of Full-Span, Trailing-Edge Flaps
Harper, John J.
October 1951
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