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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.

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At least 1,009 records · Page 56

All sources NASA NTRS DOE OSTI

NASA NTRS1951

Investigation by the transonic-bump method of a 35 degree sweptback semispan model equipped with a flap operated by a series of servovanes located ahead of and geared to the flap

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Phillips, William H↗

NASA NTRS1952

Effects of the Spanwise, Chordwise and Vertical Location of an External Store on the Aerodynamic Characteristics of a 60 Degree Delta Wing at Mach Numbers of 1.41, 1.62, and 1.96

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Jacobsen, Carl R↗

NASA NTRS1952

A study of the flow field behind the triangular horizontal tail of a canard airplane at approximately the vertical-tail location by means of a tuft grid

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Johnson, Joseph L , Jr↗

NASA NTRS1952

Some low-speed studies of the effects of wing location on wing-deformation-body-freedom flutter

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Widmayer, E , Jr↗

NASA NTRS1953

Low-speed longitudinal characteristics of an unswept hexagonal wing with and without a fuselage and a horizontal tail located at various positions at Reynolds numbers from 2.8 x 10(exp 6) to 7.6 x 10(exp 6)

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Foster, Gerald V↗

NASA NTRS1953

A Transonic Wind-tunnel Investigation of the Effects of Longitudinal Wing Location and Varying Body Size on the Interference Characteristics of a 45 Degrees Sweptback Wing

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Loving, Donald L↗

NASA NTRS1953

Investigation at Transonic Speeds of a Forward-located Underslung Air Inlet on a Body of Revolution

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Pierpont, P Kenneth↗

NASA NTRS1953

Effects of span and spanwise and chordwise location on the control effectiveness of spoilers on a 50 degree sweptback wing at Mach numbers of 1.41 and 1.96

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Kindell, William H↗

NASA NTRS1952

Characteristics of flap-type spoiler ailerons at various locations on a 60 degree delta wing with a double slotted flap

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Croom, Delwin R↗

NASA NTRS1953

Effect of Circumferential Location on Angle of Attack Performance of Twin Half-conical Scoop-type Inlets Mounted Symmetrically on the RM-10 Body of Revolution

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Valerino, Alfred S↗

NASA NTRS1953

The Calculated and Experimental Incremental Loads and Moments Produced by Split Flaps of Various Spans and Spanwise Locations on a 45 Degrees Sweptback Wing of Aspect Ratio 8

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Kelly, H Neale↗

NASA NTRS1953

Effect of fuel injector location and mixture control on performance of a 16-inch ram-jet can-type combustor

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Cervenka, A J↗

NASA NTRS1942

Ground effect on downwash angles and wake location

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Katzoff, S↗

NASA NTRS1953

Low-speed investigation of the effects of location of a delta horizontal tail on the longitudinal stability and control of a fuselage and thin delta wing with double slotted flaps including the effects of a ground board

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Riebe, John M↗

NASA NTRS1953

Transonic Flight Tests to Determine Zero-lift Drag and Pressure Recovery of Nacelles Located at the Wing Root on a 45 Degree Sweptback Wing and Body Configuration

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Hoffman, Sherwood↗

NASA NTRS1953

Investigation of Spoilers at a Mach Number of 1.93 to Determine the Effects of Height and Chordwise Location on the Section Aerodynamic Characteristics of a Two-dimensional Wing

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Mueller, James N↗

NASA NTRS1953

Low-speed longitudinal characteristics of two unswept wings of hexagonal airfoil sections having aspect ratios of 2.5 and 4.0 with fuselage and with horizontal tail located at various vertical positions

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Hadaway, William M↗

NASA NTRS1951

Effect of horizontal-tail location on low-speed static longitudinal stability and damping in pitch of a model having 45 degrees sweptback wing and tail surfaces

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Lichtenstein, Jacob H↗