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J Richard Spahr

Observed names: J. Richard Spahr, Spahr, J Richard, Spahr, J. R., Spahr, J. Richard, Spahr, J. Richard.
OpenAlex ID: A5033719325
Wind-tunnel Investigation of the Vortex Wake and Downwash Field Behind Triangular Wings and Wing-body Combinations at Supersonic Speeds
1953 · J Richard Spahr, R. DICKEY · NASA STI Repository (National Aeronautics and Space Administration) · 5
Effect of tail surfaces on the base drag of a body of revolution at Mach numbers of 1.5 and 2.0
1951 · J Richard Spahr, R. DICKEY · Defense Technical Information Center (DTIC) · 5
Comparison of the effectiveness of flares with that of fins for stabilizing low fineness ratio bodies at Mach numbers from 0.6 to 5.8
1962 · L. H. Jorgensen, J Richard Spahr, et al. · NASA Technical Reports Server (NASA) · 2
Contribution of the Wing Panels to the Forces and Moments of Supersonic Wing-body Combinations at Combined Angles
1958 · J Richard Spahr · NASA STI Repository (National Aeronautics and Space Administration) · 2
Longitudinal aerodynamic characteristics to large angles of attack of a cruciform missile configuration at a Mach number of 2
1954 · J Richard Spahr · NASA STI Repository (National Aeronautics and Space Administration) · 2
Lateral-control characteristics of various spoiler arrangements as measured in flight
1947 · J Richard Spahr · NASA STI Repository (National Aeronautics and Space Administration) · 2
Aerodynamics of bodies, wings, and wing-body combinations at high angles of attack and supersonic speeds
1956 · Jack N. Nielsen, J Richard Spahr, et al. · 1
Wind-tunnel investigation at Mach numbers of 1.5 and 2.0 of a canard missile configuration
1951 · J Richard Spahr, R. A. Robinson · NASA STI Repository (National Aeronautics and Space Administration) · 1
Static and dynamic longitudinal stability of missiles
2011 · J Richard Spahr, Murray Tobak
The pioneer projects: Economical exploration of the solar system
1975 · J Richard Spahr, C. F. Hall
Aerodynamic Loads on Tails at High Angles of Attack and Sideslip
1957 · Edward C Polhamus, J Richard Spahr · NASA STI Repository (National Aeronautics and Space Administration)
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Theoretical investigation of the effects of configuration changes on the center of pressure shift of a body-wing-tail combination due to angle of attack and Mach number at transonic and supersonic speeds
1955 · J Richard Spahr · NASA STI Repository (National Aeronautics and Space Administration)
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Wind-Tunnel Investigation of a 1/60-Scale Model of the Republic MX-1554 Airplane at a Mach Number of 2.85
1953 · R. DICKEY, J Richard Spahr
NACA Research Memorandums
1953 · Dickey, Robert R., Spahr, J. Richard · University of North Texas Digital Library (University of North Texas)
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Wind-tunnel investigation at Mach numbers of 2.0 and 2.9 of several configurations of a supersonic ram-jet test vehicle
1950 · J Richard Spahr, R. A. Robinson · NASA STI Repository (National Aeronautics and Space Administration)
NACA Research Memorandums
1950 · Spahr, J. Richard, Polhamus, Edward C. · University of North Texas Digital Library (University of North Texas)
PDF
A Supersonic Ram-jet Test Vehicle a Supersonic Ram-jet Test Vehicle
1950 · J Richard Spahr, Robert A. Robinson
NACA Technical Notes
1947 · Spahr, J. Richard, Dickey, Robert R. · University of North Texas Digital Library (University of North Texas)
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Measurements in Flight of the Lateral-Control Characteristics of an Airplane Equipped with Full-Span Zap Flaps and Simple Circular-Arc-Type Ailerons
1944 · Don R. Christophersen, J Richard Spahr
NACA Memorandum Reports
1943 · Spahr, J. Richard, Christophersen, Don R. · University of North Texas Digital Library (University of North Texas)
Works count: 32
Citation count: 20
H-index: 2
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