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Wind-Tunnel Investigation of the Static Longitudinal Stability Characteristics of a 0.15-Scale Model of the Hermes A-1E2 Missile at High Subsonic Mach Numbers
Date: September 11, 1952
Creator: Alford, William J., Jr.
Description: The static longitudinal stability characteristics of a 0.15-scale model of the Hermes A-lE2 missile have been determined in the Langley high-speed 7- by 10-foot tunnel over a Mach number range of 0.50 to 0.98, corresponding to Reynolds numbers, based on body length, of 12.3 x 10(exp 6) to 17.1 x 10(exp 6). This paper presents results obtained with body alone and body-fins combinations at 0 degrees (one set of fins vertical and the other set horizontal) and 45 degree angle of roll. The results indicate that the addition of the fins to the body insures static longitudinal stability and provides essentially linear variations of the lift and pitching moment at small angles of attack throughout the Mach number range. The slopes of the lift and pitching-moment curves vary slightly with Mach number and show only small effects due to the angle of roll.
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc64720/
A wind-tunnel investigation of the static stability characteristics of a 1/8-scale ejectable pilot-seat combination at a Mach number of 0.8
Date: December 7, 1951
Creator: Visconti, Fioravante
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc58983/
Wind-tunnel investigation of the use of leading-edge and trailing-edge area-suction flaps on a 13-percent-thick straight wing and fuselage model
Date: January 24, 1958
Creator: Holzhauser, Curt A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc63996/
A wind-tunnel investigation of the use of spoilers for obtaining static longitudinal stability of a canard-missile model in reverse flight
Date: June 21, 1954
Creator: Fletcher, Herman S
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc60160/
Wind-tunnel investigation of the vortex wake and downwash field behind triangular wings and wing-body combinations at supersonic speeds
Date: June 25, 1953
Creator: Spahr, J Richard
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc59797/
A Wind-tunnel Investigation of the Wing Loads Due to Deflected Inboard Ailerons on a 45 Deg Sweptback Wing at Transonic Speeds
Date: July 21, 1958
Creator: Heath, A. R., Jr.
Description: Effects of deflected inboard ailerons on wing loads of 45-deg swept-back wing at transonic speeds.
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc52884/
A wind-tunnel investigation of the wing loads due to deflected inboard ailerons on a 45 degree sweptback wing at transonic speeds
Date: July 21, 1958
Creator: Heath, Atwood R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc64262/
Wind-tunnel investigation of transonic aileron flutter
Date: June 9, 1949
Creator: Erickson, Albert L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc58213/
Wind-tunnel investigation of transonic aileron flutter of a semispan wing model with an NACA 23013 section
Date: July 12, 1948
Creator: Perone, Angelo
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc57775/
Wind-tunnel investigation of trimming tabs on a thickened and beveled aileron on a tapered low-drag wing
Date: March 1, 1943
Creator: Crandall, Stewart M
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc61413/