Author

Charles F Whitcomb

Observed names: Charles F. Whitcomb, Whitcomb, C. F., Whitcomb, Charles F, Whitcomb, Charles F.

Observed institution: Langley Research Center

OpenAlex ID: A5086272264

Pressure distributions on three bodies of revolution to determine the effect of Reynolds number up to and including the transonic speed range

1953 · John M Swihart, Charles F Whitcomb · University of Florida Digital Collections (University of Florida) · 7

Air-flow and power characteristics of the Langley 16-foot transonic tunnel with slotted test section

1952 · Vernon G Ward, Charles F Whitcomb, et al. · NASA Technical Reports Server (NASA) · 5

Subsonic and transonic pressure distributions around a bluff afterbody in the wake of a 120 deg cone for various separation distances

1971 · J. W. Sawyer, Charles F Whitcomb · NASA Technical Reports Server (NASA) · 2

An Experimental Investigation of Boundary Interference on Force and Moment Characteristics of Lifting Models in the Langley 16- and 8-foot Transonic Tunnels

1953 · Charles F Whitcomb, Robert S. Osborne · 2

Transonic Investigation of Aerodynamic Characteristics of a Swept-Wing Fighter-Airplane Model with Leading-Edge Droop in Combination with Outboard Chord-Extensions and Notches

1961 · Charles F Whitcomb, H. T. Norton · Defense Technical Information Center (DTIC) · 1

Transonic investigation of aerodynamic characteristics of a swept-wing fighter-airplane model with leading-edge droop in combination with outboard chord-extensions and notches /

1961 · Whitcomb, Charles F., Norton, Harry T., et al. · University of Michigan Library Repository

An Investigation of Wing and Aileron Loads Due to Deflected Inboard and Outboard Ailerons on a 4-Percent-Thick 30 deg Sweptback Wing at Transonic Speeds

1961 · Charles F Whitcomb, Chris C Critzos, et al. · NASA Technical Reports Server (NASA)

Static stability and control characteristics of two large-dihedral right triangular pyramid lifting reentry configurations at a Mach number of 3.05

1960 · W. E. Foss, Charles F Whitcomb · NASA STI Repository (National Aeronautics and Space Administration)

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Transonic characteristics of outboard ailerons on a 4-percent-thick 30 degree sweptback wing, including some effects of aileron trailing-edge thickness and aerodynamic balance

1958 · Charles F Whitcomb, Chris C Critzos

Aerodynamic Load Distribution on a 45 Degree Sweptback Wing with Leading-edge Chord-extensions at Transonic Speeds, Including Effects of a Spoiler-slot-deflector Aileron

1958 · James W Schmeer, Charles F Whitcomb, et al.

Aerodynamic load distribution over a 45 degree swept wing having a spoiler-slot-deflector aileron and other spoiler ailerons for Mach numbers from 0.60 to 1.03

1957 · F E West, Charles F Whitcomb, et al.

Effectiveness at Transonic Speeds of Flap-type Ailerons for Several Spanwise Locations on a 4-percent-thick Sweptback-wing--fuselage Model with and Without Tails

1957 · Gerald Hieser, Charles F Whitcomb

Research Memorandum. Effectiveness at Transonic Speeds of Flap-type .> Ailerons for Several Spanwise Locations on a 4-percent-thick Sweptback-wing-fuseiage Model With and Without Tails

1957 · Gerald Hieser, Charles F Whitcomb

Investigation of spoiler-slot-deflector ailerons and other spoiler ailerons on a 45 degree sweptback-wing--fuselage combination at Mach numbers from 0.60 to 1.03

1956 · F E West, Charles F Whitcomb, et al. · NASA STI Repository (National Aeronautics and Space Administration)

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Drag Investigation of a Swept-wing Fighter-airplane Model Incorporating Two Drag-rise-reducing Fuselage Revisions

1955 · Charles F Whitcomb, Edwin E Lee

NACA Research Memorandums

1955 · Schmeer, James W., Whitcomb, Charles F., et al. · University of North Texas Digital Library (University of North Texas)

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NACA Research Memorandums

1953 · Whitcomb, Charles F., Osborne, Robert S. · University of North Texas Digital Library (University of North Texas)

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An NACA Transonic Test Section with Tapered Slots Tested at Mach Numbers to 1.26

1950 · Vernon G Ward, Charles F Whitcomb, et al.

NACA Research Memorandums

1950 · Ward, Vernon G., Whitcomb, Charles F., et al. · University of North Texas Digital Library (University of North Texas)

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Investigation of the Effects of a Nacelle on the Aerodynamic Characteristics of a Swept Wing and the Effects of Sweep on a Wing Alone

1948 · Gerald Hieser, Charles F Whitcomb · Defense Technical Information Center (DTIC)

NACA Technical Notes

1948 · Hieser, Gerald, Whitcomb, Charles F. · University of North Texas Digital Library (University of North Texas)

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Works count: 35

Citation count: 17

H-index: 2

I10-index: