An investigation of several NACA 1-series inlets at Mach numbers from 0.4 to 1.29 for mass-flow ratios near 1.0 /

Investigation of two bifurcated-duct inlet systems from Mach 0 to 2.0 over a wide range of angles of attack /
by: Latham, Eldon A.
Published: (1976)

Boundary-layer bleed system study for a full-scale, mixed-compression inlet with 45 percent internal contraction /
by: Shaw, Robert J. (Robert Joseph), 1946-, et al.
Published: (1976)

Turbulent boundary-layer studies at high Reynolds numbers at Mach numbers between 0.2 and 2.8 /
by: Winter, K. G.
Published: (1973)

Mach number measurements in high-speed wind tunnels /
by: Hill, Jacques A. F.
Published: (1956)

In-flight boundary-layer measurements on a hollow cylinder at a Mach number of 3.0 /
by: Quinn, Robert D., et al.
Published: (1980)

A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-Meter Transonic Cryogenic Tunnel /
by: Lawing, Pierce L., et al.
Published: (1980)

Measurement of the internal drag of air breathing installations on slender wing-body combinations at supersonic speeds /
by: Britton, J. W.
Published: (1967)

Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients /
by: Sanders, Bobby W.
Published: (1980)

Measurements of fluctuating pressures in 8- by 6-foot supersonic wind tunnel for Mach number range of 0.56 to 2.07 /
by: Karabinus, Raymond J., et al.
Published: (1970)

Papier mâché /
by: Haines, Susanne
Published: (1990)

Creative papier mache.
by: Lorrimar, Betty
Published: (1971)

Aeroacoustics of low mach number flows fundamentals, analysis, and measurement /
by: Glegg, Stewart A. L., et al.
Published: (2023)

Aeroacoustics of low mach number flows fundamentals, analysis, and measurement /
by: Glegg, Stewart A. L., et al.
Published: (2023)

Aeroacoustics of low mach number flows fundamentals, analysis, and measurement /
by: Glegg, Stewart A. L., et al.
Published: (2023)

Noise suppression by an acoustically treated three-ring inlet on a TF-34 engine /
by: Minner, Gene L., et al.
Published: (1976)

Papier-mache /
by: Rumpf, Betty
Published: (1973)

Mach number correlation for a two-dimensional helicopter rotor-blade analysis in the tip region /
by: Schillings, John Joseph, 1958-
Published: (1983)

Aeroacoustics of low Mach number flows : fundamentals, analysis, and measurement /
by: Glegg, Stewart A. L., et al.
Published: (2017)

Mach bands : quantitative studies on neural networks in the retina.
by: Ratliff, Floyd
Published: (1965)

Creating with papier-mache /
by: Seidelman, James E.
Published: (1971)

Thrust performance of isolated two dimension suppressed plug nozzles with and without ejectors at mach numbers from 0 to 0.45 /
by: Harrington, Douglas E., et al.
Published: (1976)

Supersonic transport optimization to Mach 4 /
by: Bushnell, Dennis M.
Published: (2021)

Papier mache /
by: McLaughlin, Terence
Published: (1975)

Mach 5 inlet CFD and experimental results /
by: Weir, Lois J.
Published: (1989)

Mach 5 inlet CFD and experimental results /
by: Weir, Lois J.
Published: (1989)

Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20 /
by: Carson, George T., et al.
Published: (1988)

Flight Mechanics/Estimation Theory Symposium, 1989 : proceedings of a symposium sponsored by NASA Goddard Space Flight Center and held at Goddard Space Flight Center, Greenbelt, Maryland, May 23-24, 1989 /
Published: (1989)

Analysis of experimental data for cast 10-2/DOA2 supercritical airfoil at high Reynolds numbers = Analyse de données expérimentales pour le plan supercritique cast 10-2/DOA2 en fonction de nombres de Reynolds élevés /
by: Chan, Y. Y.
Published: (1988)

Analysis of experimental data for cast 10-2/DOA 2 supercritical airfoil at low Reynolds numbers and application to high Reynolds number flow = Analyse des données expérimentales de l'aile supercritique cast 10-2/DOA 2 aux faibles nombres de Reynolds et application des résultats aux simulations d'écoulement à des nombres de Reynolds élevés /
by: Chan, Y. Y.
Published: (1989)

Mach number dependence of the coherent structure in high speed subsonic jets /
by: Whitaker, Kevin William, 1957-
Published: (1982)

The effect of base bleed on the base pressure of several shrouded and unshrouded propelling nozzles at M [infinity] = 1.96 /
by: Shaw, M. M.
Published: (1967)

Experimental aeroheating study in NASA LaRC 20-Inch Mach 6 air tunnel : discrete roughness on BOLT -- test 7071 /
by: Berry, Scott A., et al.
Published: (2023)

Effects of wing sweep on boundary-layer transition for a smooth F-14A wing at Mach numbers from 0.700 to 0.825 /
by: Anderson, Bianca T. (Bianca Trujillo)
Published: (1990)

Design in papier mache /
by: Kenny, Carla
Published: (1971)

Papier-mache artistry /
by: Meilach, Dona Z.
Published: (1971)

The art of paper mache /
by: Kenny, Carla
Published: (1968)